Citation
List of reports with prices

Material Information

Title:
List of reports with prices
Creator:
United States -- National Advisory Committee for Aeronautics
Place of Publication:
Washington, D.C.
Publisher:
U.S. G.P.O.
Publication Date:
Frequency:
irregular
Language:
English
Physical Description:
v. : ; 19 cm.

Subjects

Subjects / Keywords:
Aeronautics -- Bibliography -- Periodicals ( lcsh )
Government publications -- Bibliography -- Periodicals -- United States ( lcsh )
Genre:
bibliography ( marcgt )
federal government publication ( marcgt )

Notes

Dates or Sequential Designation:
May 1, 1926-
General Note:
Title from cover.
Statement of Responsibility:
National Advisory Committee for Aeronautics.

Record Information

Source Institution:
University of Florida
Rights Management:
This item is a work of the U.S. federal government and not subject to copyright pursuant to 17 U.S.C. §105.
Resource Identifier:
030814821 ( ALEPH )
10739617 ( OCLC )
Classification:
Z5063 .U64 ( lcc )
016.62913 U62 ( ddc )

Full Text














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NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS





LIST OF REPORTS
WITH PRICES



EDITION JANUARY 1936


UNITED STATES
GOVERNMENT PRINTING OFFICE
WASHINGTON : 196











NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS


NOTE
This is a list of the Reports of the National Advisory Com-
mittee for Aeronautics prepared as of January 1936, arranged
by subjects.
Unless otherwise indicated, all reports may be obtained at
the prices stated from the Superintendent of Documents, Gov-
ernment Printing Office, Washington, D.C. (See "Instruc-
tions for the Purchase of Government Publications" below.)
All reports marked as out of print are available for reference
or loan upon application to the Office of Aeronautical
Intelligence, National Advisory Committee for Aeronautics.
Washington, D.C.

INSTRUCTIONS FOR THE PURCHASE OF GOVERNMENT
PUBLICATIONS
Reports may be purchased on application to the Superin-
tendent of Documents, Government Printing Office, Waahington.
D.C., which should be accompanied by remittance in the form
of coupons, postal money order, express order, or certified
check. If currency is sent, it will be at sender's risk. Foreign
orders should be accompanied by international money order
or draft on an American bank. Postage stamps, foreign money,
defaced or smooth coins, will not be accepted.
Beginning with No. 508, a subscription for the Committee's
Technical Reports may be placed with the Superintendent of
Documents. Domestic rate, $3 a year; foreign rate, $4.26 a
year.
(in)



















Digitized by the Internet Archive
in 2013













http://archive.org/detail Is/listofrepo1936unit

















INDEX
Page
Annual reports--------------------------------- I
Bibliographies------------------------------------- 1
Technical reports--------------------------------- 3
Aerodynamics --------------------------------- 3
Airfoils and wing sections----------------------- 6
Airplanes-Full-scale experiments --------------- 11
Airplanes-Model experiments----------------- 16
Airships------------------------------------- 21
Autogiros-See rotor planes--------------------- 48
Engines and accessories------------------------- 23
Fuels---------------------------------------- 34
Gases---------------------------------------- 35
Helicopters ----------------------------------- 36
Hydrodynamics ------------------------------- 36
Instruments --------------------------------- 36
Materials ------------------------------------- 40
Meteorology---------------------------------- 42
Miscellaneous --------------------------------- 43
Nomenclature--------------------------------- 43
Parachutes ------------------------------------ 44
Propellers ------------------------------------- 44
Rotor planes---------------------------------- 48
Seaplanes------------------------------------- 48
Stability and control--------------------------- 49
Strength of construction------------------------ 51
Wind tunnels and laboratories------------------- 53
(v)











NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS

ANNUAL REPORTS


First 1-------
Second 1
Third1
Fourth
Fifth ------
Sixth -------
Seventh I - -
Eighth '
Ninth I------
Tenth1------
Eleventh 1.
Twelfth I----
Thirteenth 1
Fourteenth---
Fifteenth--....--
Sixteenth..-- -
Seventeenth--
Eighteenth - _
Nineteenth _ -
Twentieth - -


Year

1915
1916
1917
1918
1919
1920
1921
1922
1923
1924
1925
1926
1927
1928
1929
1930
1931
1932
1933
1934


With
With
With
With
With
With
With
With
With
With
With
With
With
With
With
With
With
With
With
With


Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports


Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.


I Price

1-7_
8-12 ------------
13-23. .
24-50---- ------
51-82----- ------
83-110 ----------
111-132-..-.....------
133-158---,----
159-185--L -----
186-209--------
210-232----
233-256.---------
257-282---------
283-308 --- $1.25
309-336--- 2.35
337-364.--- 3.00
365-400--. 3.00
401-440--- 2.50
441-474-_- 2.50
475-507.--- 2.75


I Out of print. Available for reference or loan in the Officeof Aeronautical Intel
ligence, National Advisory Committee for Aeronautics, and in the libraries of large
cities.
NoTE.-Beginning with the sixteenth, the annual reports are to be bound in buck.
ram only.
BIBLIOGRAPHIES


Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography


Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics


(1909-1916).-------. .
(1917-1919)-------------
(1920-1921)------------i
(1922)------------------
(1923)-------------------
(1924)-..---..---------
(1925)
(1926)------------................
(1927) ....-------------------
(1928)-------------------
(1929)-----------------
(1930).-----------------
(1931)-----------------


(11


$2.00
.75
.35
.25
.25
.25
.50
20
.35
.50
35
.50
.50











TECHNICAL REPORTS


AERODYNAMICS


Title


1 12

20

3 78

S79
3 83


97

3114

8116

139

144

3151

3185

3 197


I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
SOut of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.


No.


Experimental Researches on the Resistance of
Air. By L. Marchis. (Second Annual, 1916) ------
Aerodynamic Coefficients and Transformation
Tables. By Joseph S. Ames. (Third Annual,
1917)--------------------------------- $0.05
The Limiting Velocity in Falling from a Great
Height. By Edwin Bidwell Wilson. (Fifth
Annual, 1919)----------------------------------
Bomb Trajectories. By Edwin Bidwell Wilson.
(Fifth Annual, 1919)--------------------------
Wind Tunnel Studies in Aerodynamic Phe-
nomena at High Speed. By F. W. Caldwell
and E. N. Fales. (Sixth Annual, 1920)-----------
General Theory of the Steady Motion of an
Airplane. By George de Bothezat. (Sixth
Annual, 1920)---------------------------- .15
Some New Aerodynamical Relations. By Max
M. Munk. (Seventh Annual, 1921) -------
Applications of Modern Hydrodynamics to
Aeronautics. By L. Prandtl. (Seventh An-
nual, 1921)---------------------------------
Influence of Model Surface and Air Flow Tex-
ture on Resistance of Aerodynamic Bodies.
By A. F. Zahm. (Eighth Annual, 1922).----- 05
The Decay of a Simple Eddy. By H. Bateman.
(Eighth Annual, 1922)--------------------- .05
General Biplane Theory. By Max M. Munk.
(Eighth Annual, 1922)--- ---------------
The Resistance of Spheres in Wind Tunnels
and in Air. By David L. Bacon and Elliott
G. Reid. (Ninth Annual, 1923)------------ ------
A New Relation Between the Induced Yawing
Moments and the Rolling Moments of an
Airfoil in Straight Motion. By Max M.
Munk. (Tenth Annual 1924)--------------


Price










AERODYNAMICS-Continued


No.

213

'247

1253

287

289

311

316

323

335

349


361



362

395


I Out of print. Available as a separate report for reference or loan In the Office
of Aeronautical Intelligence. National Advisory Committee for Aeronautics.


Title

A Resum6 of the Advances in Theoretical
Aeronautics Made by Max M. Munk. By
Joseph S. Ames. (Eleventh Annual, 1925) ----
Pressure of Air on Coming to Rest from Various
Speeds. ByA.F.Zahm. (Twelfth Annual, 1926)_
Flow and Drag Formulas for Simple Quadrics.
By A. F. Zahm. (Twelfth Annual, 1926)----.
Theories of Flow Similitude. By A. F. Zahm.
(Fourteenth Annual, 1928)---------------
Forces on Elliptic Cylinders in Uniform Air
Stream. By A. F. Zahm, R. H. Smith, and
F. A. Louden. (Fourteenth Annual, 1928).--
Aerodynamic Theory and Test of Strut
Forms-I. By R. H. Smith. (Fifteenth
Annual, 1929) -----------------------
Tables for Pressure of Air on Coming to Rest
from Various Speeds. By A. F. Zahm and
F. A. Louden. (Fifteenth Annual, 1929)._
Flow and Force Equations for a Body Revolv-
ing in a Fluid. By A. F. Zahm. (Fifteenth
Annual, 1929) ----------
Aerodynamic Theory and Test of Strut Forms.
Part II. By R.H. Smith. (Fifteenth Annual,
1929)-------------------------------
A Proof of the Theorem Regarding the Distribu-
tion of Lift over the Span for Minimum In-
duced Drag. By W. F. Durand. (Sixteenth
Annual, 1930)-------------------------
Experimental Determination of Jet Boundary
Corrections for Airfoil Tests in Four Open
Wind Tunnel Jets of Different Shapes. By
Montgomnerv Knight and Thomas A. Harris.
(Sixteenth Annual, 1930)..-------------
An Extended Theory of Thin Airfoils and Its
Application to the Biplane Problem. By
Clark B. Millikan. (Sixteenth Annual, 1930)_
A New Principle of Sound Frequency Analysis.
By Theodore Theodorscn. (Seventeenth An-
nual, 1931)-----------------------..-


Price


$0. 15


.05

.05

.10

.05

.20

.20


.10



.20

.20


. 15








A. ERODYNAMICS- Continued

No. Title Price

411 Theory of Wing Sections of Arbitrary Shape.
By Theodore Theodorsen. (Eighteenth An-
nual, 1932) ------------------------------$0. 10
Relation Between Aeronautic Research and Air-
craft Design. By Joseph S. Ames. (Appen-
dix to Administrative Report, 1923)--------- 15
452 General Potential Theo)ry of Arbitrary Wing
Sections. By T. Theodorsen and I. E. Gar-
rick. (Nineteenth Annual, 1933)----------- 10
465 Determination of the Theoretical Pressure Dis-
tribution for Twenty Airfoils. By I. E. Gar-
rick. (Nineteenth Annual, 1933)' --- ------ .05
496 General Theory of Aerodynamic Instability
and the Mechanism of Flutter. By Theodore
Theodorsen. (Twentieth Annual,'1934)------ .10
497 Computation of the Two-Dimensional Flow in
a Laminar Boundray Layer. By Hugh L.
Dryden. (Twentieth Annual, 1934)--------- .05
504 On the Theory of Laminar Boundary Layers
Involving Separation. By Th. von Karman
and C. B. Millikan. (Twentieth Annual,
1934)------------------------------------ .10
516 Potential Flow About Elongated Bodies of
Revolution. By Carl Kaplan. (Twenty-
First Annual, 1935)------------------------ 10
526 Noise from Two-Blade Propellers. By E. Z.
Stowell and A. F. Deming. (Twenty-First
Annual, 1935)--------------------- ----- .05
527 Air Flow in a Separating Laminar Boundary
Layer. By G. B. Schubauer. (Twenty- I
First Annual, 1935)------------------------ .05
542 Potential Flow About Arbitrary Biplane Wing
Sections. By I. E. Garrick. (Twenty-Sec-
ond Annual, 1936)------------------------------
546 The Effect of Turbulence on the Drag of Flat
Plates. By G. B. Schubauer and H. L. Dry-
den. (Twenty-Second Annual, 1936)--------- .05










AIRFOILS AND WING SECTIONS

No. Title Price

I IS Aerofoils and Aerofoil Structural Combinations.
By Edgar S. Gorrell and H. S. Martin.
j(Third Annual, 1917) ----------------
328 An Introduction to the Study of the Laws o; Air
Resistance of Aerofoils. By George de
Bothezat. (Fourth Annual, 1918)-----------
3 75 The Aerodynamic Properties of Thick Aerofoils
Suitable for Internal Bracing. By F. H.
Norton. (Fifth Annual, 1919)----------------
1 77 The Parker Variable Camber Wing. By H. F.
Parker. (Fifth Annual, 1919)------------------
1 93 Aerodynamic Characteristics of Airfoils. By
National Advisory Committee for Aero-
nautics. (Sixth Annual. 1920)
S11l The Variation of Airfoil Lift and Drag Coeffi-
cients with Changes in Size and Speed. By
W. S. Diehl. (Seventh Annual, 1921)------ ------
'121 The Minimum Induced Drag of Airfoils. By
Max M. Munk. (Seventh Annual, 1921) ---
124 Aerodynamic Characteristics of Airfoils-II.
By the National Advisory Committee for
Aeroi.autics. (Seventh Annual. 1921) ------- $0. 30
3142 General Theory of Thin Wing Sections. Bv
Max M. Munk. (Eighth Annual, 1922) ------
1 150 Pressure Distribution over Thick Aerofoils-
Model Tests. By F. H. Norton and D. L.
Bacon. (Eighltlh Annual. 1922-- ---------
s 152 The Aerodynamic Properties of Thick Aero-
foils-II.'By F. H1. Norton and D. L.
Bacon. (Eighth Annual, 1922)-------------
3 169 The Effect of Airfoil Thickness and Plan Form
on Lateral Control. By H. I. Hoot. (Ninth
Annual, 1923) ------ -------------------- ----
1182 Aerodynamic Charactersitics of Airfoils-III.
By National Advisory Committee for Aero-
nautics. (Ninth Annual, 1923 )-------------------
S191 Elements of the Wing Section Theory and of the
Wing Theory. By Max M. Munk. (Tenth
Annual, 1924)--------------------------------
I ut of print. Annual volume aviiilable for reference or loan in the Office of
Aeronautical Intelligence, National Advisory t'onimittee for Aeronautics, and
in the libraries of large cities.
I Out of print. Available as a separate report for reference or loan in the Office of
Aeroniiutical iniilligrwie. National Alvisry Committee for Aeronautics.










AIRFOILS AND WING SECTIONS-Continued


Title


200

3201

207

217


1221


229


* 233


'244

255

267

271


278

285


I Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.


No.


Price


Some Problems on the Lift and Rolling Mo-
ments of Airplane Wings. By Jas. B. Scar- i
borough. (Tenth Annual, 1924)-----------
The Effects of Shielding the Tips of Airfoils.
By Elliott G. Reid. (Tenth Annual, 1924)_._
Aerodynamic Characteristics of Airfoils at High
Speeds. By L. J. Briggs, G. F. Hull, and
H. L. Dryden. (Tenth Annual, 1924)----
Preliminary Wing Model Tests in the Variable
Density Wind Tunnel of the National Advi-
sory Committee for Aeronautics. By Max M.
Munk. (Eleventh Annual, 1925)-----------
Model Tests with a Systematic Series of 27
Wing Sections at Full Reynolds Number.
By Max M. Munk and Elton W. Miller.
(Eleventh Annual, 1925)--------------------
Pressure Distribution over Thick, Tapered Air-
foils, N. A. C. A. 81, U. S. A. 27 C Modified
and U. S. A. 35. By Elliott G. Reid.
(Eleventh Annual, 1925)-------------------
The Aerodynamic Characteristics of Seven Fre-
quently Used Wing Sections at Full Reynolds
Number. By Max M. Munk and Elton W.
Miller. (Twelfth Annual, 1926)------------
Aerodynamic Characteristics of Airfoils-IV.
By National Advisory Committee for Aero-
nautics (Twelfth Annual, 1926)-----------
Pressure Distribution over Airfoils at High
Speeds. By L. J. Briggs and H. L. Dryden.
(Twelfth Annual, 1927)--------------------
Drag of Wings with End Plates. By Paul E.
Hemke. (Thirteenth Annual, 1927)---------
Pressure Distribution Tests on PW-9 Wing
Models Showing Effects of Biplane Interfer-
ence. By A. J. Fairbanks. (Thirteenth
Annual, i927)----------------------------
Lift, Drag, and Elevator Hinge Moments of
Handley-Page Control Surfaces. By R. H.
Smith. (Thirteenth Annual, 1927)----------
A Study of Wing Flutter. By A. F. Zahm and
R. M. Bear. (Fourteenth Annual, 1928) -..---


$0. 10


.10


.10


. 10


. 15

.10


.10

.10


.15








S

AIRFOILS AND WING SECTIONS-Continued

No. Title Price

286 Aerodynamic Characteristics of Airfoils-V.
By National Advisory Committee for Aero-
nautics. (Fourteenth Annual, 1928)-------- $0.25
2S8 Pressure Distribution over a Rectangular Mono-
plane Wing Model up to 90 Angle of Attack.
By Montgomery Knight and Oscar Loeser, jr.
(Fourteenth Annual, 1928)--------------- 10
309 Joint Report on Standardization Tests on
N. P. L. R. A. F. 15 Airfoil Model. By
Walter S. Diehl. (Fifteenth Annual, 1929)--, 10
312 The Prediction of Airfoil Characteristics. By
George J. Higgins. (Fifteenth Annual, 1929). 10
315 Aerodynamic Characteristics of Airfoils-VI.
By National Advisory Committee for Aero-
nautics. (Fifteenth Annual, 1929) ---------- .20
317 Wind Tunnel Tests on a Series of Wing Models
Through a Large Angle of Attack Range. Part
I, Force Tests. By Montgomery Knight and
Carl J. Wenzinger. (Fifteenth Annual, 1929). .25
319 Aerodynamic Characteristics of Twenty-four
Airfoils at High Speeds. By L. J. Briggs
and H. L. Dryden. (Fifteenth Annual, 1929)._ .15
331 Collection of Wind Tunnel Data on Commonly
Used Wing Sections. By F. A. Louden. (Fif-
teenth Annual, 1929)---------------------- 20
336 Tests of Large Airfoils in the Propeller Research
Tunnel, including Two with Corrugated Sur-
faces. By Donald 11. Wood. (Fifteenth An-
nual, 1929) --...----..-------------------------. 10
352 Large-Scale Aerodynamic Characteristics of Air-
foils as Tested in the Variable-Density Wind
Tunnel. By Eastman N. Jacobs and Ray-
niond F. Anderson. (Sixteenth Annual, 1930). .20
353 Airfoil Pressure Distribution Investigation in the
Variable-Density Wind Tunnel. By Eastman
N. Jacobs, John Stack, and Robert M. Pinker-
ton. (Sixteenth Annual, 1930) --------. 15
360 Pressure Distribution over a Symmetrical Airfoil
Section with Trailing Edge Flap. By East-
man N. Jacobs and Robert M. Pinkerton.
(Sixteenth Annual, 1930) ........---... 15








AIRFOILS AND WING SECTIONS-Continued

No. Title Price

365 Aerodynamic Characteristics of Circular-Arc
Airfoils at High Speeds. By L. J. Briggs and
H. L. Dryden. (Seventeenth Annual, 1931). $0. 10
367 Pressure Distribution over Thick, Tapered, and
Twisted Monoplane Wing Model. N.A.C.A.
81-J. Bv Carl J. Wenzinger. (Seventeenth
Annual, 1931) ---------------------------- 10
370 Effect of Variation of Chord and Span of Ailerons
on Hinge Moments at Several Angles of Pitch.
By H. B. Monish. (Seventeenth Annual,
1931)------------------------------------ .10
383 On the Theory of Wing Sections with Particular
Reference to the Pressure Distribution. By
Theodore Theodorsen. (Seventeenth Annual,
1931)----------------------------- ------- 10
385 Wind Tunnel Tests on Airfoil Boundary Layer
Control Using a Backward-Opening Slot. By
Millard J. Bamber. (Seventeenth Annual,
1931)------------------------------------ .20
391 The Aerodynamic Characteristics of Eight Very
Thick Airfoils from Tests in the Variable Den-
sity Wind Tunnel. By Eastman N. Jacobs.
(Seventeenth Annual, i931)--------------- 10
400 The Aerodynamic Characteristics of a Slotted
Clark Y Wing as Affected by the Auxiliary
Airfoil Position. By Carl J. Wenzinger and
Joseph A. Shortal. (Seventeenth Annual,
1931)------------------------------------ .15
407 The Characteristics of a Clark Y Wing Model
Equipped with Several Forms of Low-Drag
Fixed Slots. By Fred E. Weick and Carl J.
Wenzinger. (Eighteenth Annual, 1932)-- 1')
427 The Effect of Multiple Fixed Slots and a Trail-
ing-Edge Flap on the Lift and Drag of a Clark
Y Airfoil. By Fred E. Weick and Joseph
A. Shortal. (Eighteenth Annual, 1932--- .0.5
428 Wind-Tunnel Tests of a Clark Y Wing with a
Narrow Auxiliary Airfoil in Different Posi-
tions. By Fred E. Weick and Millard J.
Bamber. (Eighteenth Annual, 1932) -------- 10








10

AIRFOILS AND WING SECTIONS-Continued

No. Title Price

431 Characteristics of Clark Y Airfoils of Small
Aspect Ratios. By C. H. Zimmerman.
(Eighteenth Annual, 1932) ------ ---- $0.05
446 Airfoil Section Characteristics as Affected by
Protuberances. Bv Eastman N. Jacobs.
(Nineteenth Annual, 1933)------------ .10
449 Wing Characteristics as Affected by Protuber-
ances of Short Span. By Eastman N. Jacobs
and Albert Sherman. (Nineteenth Annual,
1933)----------------------------------- .05
460 The Characteristics of 78 Related Airfoil Sec-
tions from Tests in the Variable-Density
Wind Tunnel. By Eastman N. Jacobs, Ken-
keth E. Ward and Robert M. Pinkerton.
(Nineteenth Annual, 1933)----------------- 15
465 Determination of the Theoretical Pressure Dis-
tribution for Twenty Airfoils. By I. E. Gar-
rick. (Nineteenth Annual, 1933)----------- 05
472 Wind-Tunnel Tests on Combinations of a Wing
with Fixed Auxiliary Airfoils having Various
Chords and Profiles. By Fred E. Weick and
Robert Sanders. (Nineteenth Annual, 1933)_ .10
480 The Aerodynamic Effects of Wing Cut-Outs.
By Albert Sherman. (Twentieth Annual,
1934)----------------------------------- .05
492 Tests of 16 Related Airfoils at High Speeds. By
John Stack and Albert E. von Doenhoff.
(Twentieth Annual, 1934)------------------ 10
502 Scale Effect on Clark Y Airfoil Characteristics
from N. A. C. A. Full-Scale Wind-Tunnel
Tests. Bv Abe Silverstein. (Twentieth An-
nual, 1934)------------------------------. 10
530 Characteristics of the N. A. C. A. 23012 Airfoil
from Tests in the Full-Scale and Variable-
Density Tunnels. By Eastman N. Jacobs
and William C. Clay. (Twenty-First An-
nual, 1935)------------------------------ .05
534 Aerodynamic Characteristics of a Wing with
Fowler Flaps Including Flap Loads, Down-
wash, and Calculated Effect on Take-Off.
By Robert C. Platt. (Twenty-First Annual,
1935)----------------------------------- .10









AIRFOILS AND WING SECTIONS-Continued

No. Title Price

537 Tests in the Variable-Density Wind Tunnel of
Related Airfoils Having the Maximum Cam-
ber Unusually Far Forward. By Eastman
N. Jacobs and Robert M. Pinkerton. (Twen-
ty-First Annual, 1935)-------------------- $0.05
540 Interference of Wing and Fuselage from Tests of
209 Combinations in the N. A. C. A. Variable-
Density Tunnel. By Eastman N. Jacobs
and Kenneth E. Ward. (Twenty-First An-
nual, 1935) ------------------------------. 10
541 Aerodynamic Characteristics of Wings with
Cambered External-Airfoil Flaps, Including
Lateral Control with a Full-Span Flap. By
Robert C. Platt. (Twenty-First Annual,
1935)---

AIRPLANES-FULL-SCALE EXPERIMENTS

3 69 A Study of Airplane Ranges and Useful Loads.
By J. C. Coffin. (Fifth Annual, 1919)------------
3 70 Preliminary Report on Free Flight Tests. By
Edward P. Warner and F. H. Norton. (Fifth
Annual, 1919) ------------------------
105 Angles of Attack and Air Speeds during Maneu-
vers. By Edward P. Warner and F. H.
Norton. (Sixth Annual, 1920)-----------------
118 The Pressure Distribution over the Horizontal
Tail Surfaces of an Airplane. By F. H. Nor-
ton. (Seventh Annual, 1921) ------------
3148 The Pressure Distribution over the Horizontal
Tail Surfaces of an Airplane-III. By F. H.
Norton and W. G. Brown. (Eighth Annual.
1922)---------- --------------
3149 Pressure Distribution over the Rudder and Fin
of an Airplane in Flight. By F. H. Norton
and W. G. Brown. (Eighth Annual, 1922)--------
'154 i A Study of Taking Off and Landing an Airplane.
By. T. Carroll. (Eighth Annual, 1922)-- -----
Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.


27903-36-2










AIRPLANES-FULL-SCALE EXPERIMENTS-Continued

No. Title Price

3155 A Study of Airplane Maneuvers with Special
Reference to Angular Velocities. By H. J.
E. Reid. (Eighth Annual, 1922) ------- ----
162 Complete Study of the Longitudinal Oscillation
of a VE-7 Airplane. By F. H. Norton and
W. G. Brown. (Ninth Annual, 1923)------- $0.05
163 The Vertical, Longitudinal, and Lateral Accelera-
tions Experienced by an S-5A Airplane while
Maneuvering. B% F. H. Norton and T.
Carroll. (Ninth Annual, 1923)----------- .05
167 The Measurement of the Damping in Roll on a
JN4H in Flight. Bv F. H. Norton. (Ninth
Annual, 1923)----------------------------- .05
S170 A Study of Longitudinal Dynamic Stability in
Flight. By F. H. Norton. (Ninth Annual,
1923)f---- 7---- -----
173 Reliable Formul? for Estimating Airplane
Performance and the Effects of the Changes in
Weight, Wing Area, or Power. By Walter
S. Diehl. (Ninth Annual, 1923)---------- .05
174 The Small Angular Oscillations of Airplanes in
Steady Flight. By F. H. Norton. (Ninth
Annual, 1923)---------------------------- .05
S192 Charts for Graphical Estimation of Airplane
Performance. By Walter S. Diehl. (Tenth
Annual, 1924)---------------------------------
193 Pressure Distribution Over thie \Vings of an
MB-3 Airplane in Flight. By F. 11. Norton.
(Tenth Annual, 1924) -..-----------
a 194 Investigation of Slip Stream Velocity. By J. \V.
Crowley, jr. (Tenth Annual, 1924) ------... -----
203 Aceelerations in Fliglht. By J. H. Doolittle.
(Tenth Annual, 1924)----------. 10
219 Some Aspects of the Comparison of Model and
Full-Scale Tests. By D. W. Taylor. (Elev-
enth Annual, 1925)------------------------ 10
228 A Study of the Effect of a D)iving Start on Air-
plane Speed. By Walter S. Diehl. (Eleventh
Annual, 1925)----- ----------------------- 05
1 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence. National Alvisory CommTittee for Aeronautics











No.


234

'238

'249


257


265

293


297

304



307


364


346


13

AIRPLANES-FULL-SCALE EXPERIM ENTS-Continued

Title

Three Methods of Calculating Range and En-
durance of Airplanes. By Walter S. Diehl.
(Twelfth Annual, 1926)--------------------
The Effect of Flight Path Inclination on Airplane
Velocity. By Walter S. Diehl. (Twelfth
Annual, 1926) ----------------------------
A Comparison of the Take-off and Landing
Characteristics of a Number of Service Air-
planes. By Thomas Carroll. (Twelfth An-
nual, 1926)-------------------------------
Pressure Distribution over a Wing and Tail
Rib of a VE-7 and of a TS Airplane in Flight.
By J. W. Crowley, jr. (Thirteenth Annual,
1927)------------------------------------
A Full-Scale Investigation of Ground Effect.
By Elliott G. Reid. (Thirteenth Annual.
1927)------------------------------------
Two practical Methods for the Calculation of
the Horizontal Tail Area Necessary for a
Statically Stable Airplane. By Walter S.
Diehl. (Fourteenth Annual, 1928)----------
The Reduction of Observed Airplane Perform-
ance to Standard Conditions. By Walter S.
Diehl. (Fourteenth Annual, 1928)----------
An Investigation of the Aerodynamic Charac-
teristics of an Airplane Equipped with Several
Different Sets of Wings. By J. W. Crowley,
jr., and M. W. Green. (Fourteenth Annual,
1928)------------------------------------
The Pressure Distribution over the Horizontal
and Vertical Tail Surfaces of the F6C-4 Pur-
suit Airplane in Violent Maneuvers. By R.
V. Rhode. (Fourteenth Annual, 1928)------
Pressure Distribution over the Wings and Tail
Surfaces of a PW-9 Pursuit Airplane in Flight.
By Richard V. Rhode. (Sixteenth Annual,
1930)------------------------------
Dynamic and Flight Tests on Rubber-Cord and
Oleo-Rubber-Disk Landing Gears for an
F6C4 Airplane. By Wm. C. Peck. (Seven-
teenth Annual, 1931)---------------------


. 15


.10

S15



S10


. 10


.60


. 10


3 Out of print. Available as a separate report for reference or loan iu the Office
of Aeronautical Intelligence, National Advisory Committee for A.eroniutics.


Price


$0. 10








14

AIRPLANES-FULL-SCALE EXPERIMENTS-Continued

No. Title Price

368 A New Chart for Estimating the Absolute Ceil-
ing of an Airplane. By Walter S. Diehl.
seventeenth Annual, 1931)---------------- $0. 10
369 Maneuverability Investigation of the F6C3
Airplane with Special Flight Instruments.
By C. H. Dearborn and H. W. Kirchbaum.
Seventeenth Annual, 1931) 15
377 A Method of Flight Measurement of Spins. By
Hartley A. Soul6 and Nathan F. Scudder.
(Seventeenth Annual, 1931) -------------- .10
380 Pressure Distribution over the Fuselage of a
PW-9 Airplane in Flight. By R. V. Rhode
and E. E. Lundquist. (Seventeenth Annual,
1931)------------------------------------- .20
3bl1 Static, Drop and Flight Tests on Musselman
Type Airwheels. By Wm. C. Peck and
Albert P. Beard. (Seventeenth. Annual,
1931)---------------------------------- 15
3`6 Maneuverability Investigation of an F6C-4
Fignter Airplane. By C. H. Dearborn and
H. W. Kirschbaiim. (Seventeenth Annual,
1931)------------------ .20
403 Ice P'revention on Aircraft by Means of Engine
Exhaust Heat and a Technical Study of Heat
Transmission from a Clark Y Airfoil. By
Theodore Theodursen and William C. Clay.
Eighteenth Annual, 1932)------------------ .20
406 Drop and Flight Tests on NY-2 Landing Gears,
Including Measurements of Vertical Velocities
at Landing. By W. C. Peck and A. P. Beard.
(Eighteenth Annual, 1932)----------------- 15
40S General Formulas and Charts for the Calcula-
tion of Airplane Performance. Bv W. Bailey
Oswald. (Eighteenth Annual, 1932).--------. 25
413 A Method for Computing Leading Edge Loads.
By Richard V. Rhode and Henry A. Pearson.
(Eighteenth Annual, 1932)----------------- .10
414 The Effect on Airplane Performance of Several
Types of Low-Drag Cowling for Radial Air-
Cooled Engines. Bv Wm. H. McAvovy, Oscar
W. Schev, iard Alfred W. Young. (Eigh-
teentlt, Annual3, 1932)---------------.------- .20








15

AIRPLANES-FULL-SCALE EXPERIMENTS-Continued

No. Title Price

418 Preliminary Investigation of Modifications to
Conventional Airplanes to give Nonstalling
Sand Short-Landing Characteristics. By Fred
E. Weick. (Eighteenth Annual, 1932) ----- -$0. 05
441 A Flight Investigation of the Spinning of the
NY-1 Airplane with Varied Mass Distribu-
tion and Other Modifications, and an Analysis
Based on Wind-Tunnel Tests. By Nathan F.
Scudder. (Nineteenth Annual, 1933)-------- 10
450 The Calculation of Take-Off Run. By Walter
S. Diehl. (Nineteenth Annual, 1933,------ 05
457 Maneuverability Investigation of an "03,U-1"
Observation Airplane. By F. L. Thompson
and H. W. Kirschbaum. (Nineteenth Annual,
1933)------------------------------------ .05
458 Relative Loading on Biplane Wings. By Walter
SS. Diehl. (Nineteenth Annual, 1933)-------- 10
482 Wing-Fuselage Interference, Tail Buffeting, and
Air Flow About the Tail of a Low-Wing Mono-
plane. By James A. White and Manley J.
Hood. (Twentieth Ann ital, 1934) ----------- 10
484 A Flight Investigation of the Effect of Mass Dis-
tribution and Control Setting on the Spinning
of the XN2Y-1 Airplane. By N. F. Scudder.
(Twentieth Annual, 1934)----------------- .05
485 The Drag of Airplane Wheels, Wheel Fairings
and Landing Gears-i. By William H. Herrn-
stein, Jr., and David Biermann. (Twentieth
Annual, 1934)---------------------------- 10
489 Air Conditions Close to the Ground and the Ef-
fect on Airplane Landings. By F. L. Thomp-
son, W. C. Peck, and A. P. Beard. (Twenti-
eth Annual, 1934)------------------------- .10
494 A Flight Investigation of the Lateral Control
Characteristics of Short Wide Ailerons and
Various Spoilers with Different Amounts of
Wing Dihedral. By Fred E. Weick, Hartley
A. Soule, and Melvin N. Gough. (Twentiethi
Annual, 1934)---------------------------- 10
498 Improved Airplane Windshields to Provide
Vision in Stormy Weather. Br\ William C.
Clay. i Twentieth Annual. 1934 ----------- 10










AIRPLANES--FULL-SCALE EXPERIMENTS-Continued

No. Title Price

500 The Influence of Tip Shape on the Wing Load
Distribution as Determined by Flight Tests.
By Richard V. Rhode. (Twentieth Annual,
1934)------------------------------1 $0. 10
501 Relative Loading on Biplane Wings of Unequal
Chords. By Walter S. Diehl. (Twentieth
Annual, 1934) ---------------------------- .05
514 The Measurement of the Field of View from
Airplane Cockpits. By Melvin N. Gough.
(Twenty-First Annual, 1935)----------- 0
517 Flighlt Investigation of Lateral Control Devices
for Use with Full-Span Flaps. By H. A.
Soul6 and W. H. McAvov. (Twenty-First
Annual, 1935)----------------------- ----- 10
518 Tlhe Drag of Airplane Wheels, Wheel Fairings
and Landing Gears.-II. Nonretractable and
Partly Retractable Landing Gears. By David
Biermatin and William H. Herrnstein, Jr.
Twentv-First Annual, 1935)--------------- 10
522 TIe Drag of Airplane WVheels, Wheel Fairings
:and La(nding Gears.-III. By William H.
Herrnstein, Jr., and David Biermann.
(Twenty-First Annual, 1935)--------------- .10
529 A Flirht Investigation of the Spinning of the
F41B-2 Biplane with Various Loads and Tail
Surfaces. By N. F. Scudder and Oscar Seid-
man. ,Tweiit y-First Annual, 1935)--------- .10
539 Investigation of Full-Scale Split Trailing-Edge
Wing Flaps with Various Chords and Hinge
LoIcations. By Rudolf Wallace. (Twenty-
Fir.st A.nnual, 1935------------------------ .10

AIRPLANES-MODEL EXPERIMENTS

S74 Construction of Models for Tests in Wind Tun-
ncls. ByF.H.Norton. (Fifth Annual, 1919)----
119 The Pressure Distribution over the Horizontal
Tail Surfaces of an Airplane-IlI. By F. H.
Norton and D. L. Bacon. (Seventh Annual,
1921)----------------------- ----$0. 10
SOut (fit print Available is a separate report fur reference or loan In the Office
of Aeroniiutical IntellJience. National Ad isory (Committee for Aeronautics.










AIRPLANES-MODEL EXPERIMENTS-Continued


No.


Title


122 Preliminary Experiments to Determine Scale
and Slip Stream Effects on a 1/24 Size Model
of a JN4H Biplane. By D. L. Bacon. (Sev-
enth Annual, 1921)-----------------------
3133 The Tail Plane. By Max M. Munk. (Eighth
Annual, 1922)-------------------------
136 Damping Coefficients due to Tail Surfaces in Air-
craft. By Lynn Chu. (Eighth Annual, 1922).
137 Point Drag and Total Drag of Navy Struts No.
I Modified. By A. F. Zahm, R. H. Smith,
and G. C. Hill. (Eighth Annual, 1922).----
140 Lift and Drag Effects on Wing Tip-Rake. By
A. F. Zahm, R. M. Bear, and G. C. Hill.
(Eighth Annual, 1922)---------------------
219 Some Aspects of the Comparison of Model and
Full-Scale Tests. By D. W. Taylor. (Elev-
enth Annual, 1925)------------------------
225 The Air Forces on a Model of the Sperry Mes-
senger Airplane Without Propeller. By Max
M. Munk and Walter S. Diehl. (Eleventh
Annual, 1925)----------------------------
236 Tests on Airplane Fuselages, Floats, and Hulls.
By Walter S. Diehl. (Twelfth Annual, 1926)_
254 Distribution of Pressure over Model of the
Upper Wing and Aileron of a Fokker D-VII
Airplane. By A. J. Fairbanks. (Twelfth
Annual, 1926)----------------------------
256 The Air Forces on a Systematic Series of Biplane
and Triplane Cellule Models. By Max M.
Munk. (Twelfth Annual, 1926)-----------
260 The Effect of a Flap and Ailerons on the N. A.
C. A.-M6 Airfoil Section. By George J. Hig-
gins and Eastman N. Jacobs. (Thirteenth
Annual, 1927)---------------------------
266 Air Force and Moment of N-20 Wing with Cer-
tain Cut-Outs. By R. H. Smith. (Thir-
teenth Annual, 1927)---------------------
S269 Air Force Tests of Sperry Messenger Model
with Six Sets of Wings. By James M. Shoe-
maker. (Thirteenth Annual, 1927)----------


5 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.


Price


$0.05


.05

.05


.10


.15


.10

.15


.10

.05










AIRPLANES-MODEL EXPERIMENTS-Continued

No. Title Price

273 Wind Tunnel Tests on Autorotation and the
"Flat Spin." By Montgomery Knight.
(Thirteenth Annual, 1927) ------------------ $0. 10
279 Tests on Models of Three British Airplanes in
the Variable Density Wind Tunnel. By
George J. Iliggins, W. S. Diehl, and George
L. DeFoe. EThirteenth Annual. 1927)...-..... 15
296 Pressure Distriliution Tests on PW-9 Wing
Models from -1 through 90 Angle of At-
tack. By Oscar E. Loeser, jr. (Fourteenth
Annual, i928)---------------------------- 15
415 Tests of Nacelle-Propc!ler Combinations in Va-
rioiiu Positions with Reference to Wings.
Part 1. Thick \Ving-N. A. C. A. Cowled
Nacelle-Tractor Propeller. By Donald H.
Wood (Eighteenth Annual, 1932 --------- 1iC
417 Pressure Distribution Tests on a Series of Clark
Y Biplane Cellules \with Special Reference to
Safety. B Richard W. Noves. (Eighteenth
Annual, 1932) ----------------------------- .10
419 Wind-Tunnel Research CoImparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. I-()rdinary Ailerons on Recetangu-
lar Wings. By Fred E. Weick and Carl J.
Wenzinger. (1Eighteenth Annual, 1932) __---- 10
422 Wind-Tunnel Research Coimparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. II-Slotted Ailerons and Frise Ail-
erons. By Fred E. Weick and Richard WV.
Noyes. (Eighteenth Annual, 1932)--------- .05
423 Wind-Tunnel Research Comparing Lateral Con-
trol De\ices, Particularly at High Angles of
Attack. Ill-Ordinary Ailerons Rigged up
10 When Neutral. By Fred E. Weick and
Carl J. Wenzinger. (Eighteenth Annual,
1932) ------------------------------------ .05
424 Wind-Tunnel Research Conmparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. IV-Floating-Tip Ailerons on Rec-
tangular Wings. By Fred E. Weick and
Thomas A. Harris. (Eighteenth Annual,
1932) ------------------------------------ 10










AIRPLANES-MODEL EXPERIMENTS-Continued

No. Title Price

436 Tests of Nacelle-Propeller Combinations in Va-
rious Positions with Reference to Wings.
Part II-Thick Wing-Various Radial-Engine
Cowlings-Tractor Propeller. By Donald H.
Wood. (Eighteenth Annual, 1932) --------- $0t 10
437 The Effect of Area and Aspect Ratio on the
Yawing Moments of Rudders at Large Angles
Sof Pitch on Three Fuselages. By Hugh L.
Dryden and B? H. Monish. (Eighteenth
Annual, 1932)--------------------------- .05
439 Wind-Tunnel Research Comparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. V-Spoilers and Ailerons on Rec-
tangular Wings. By Fred E. Weick and Joseph
A. Shortal. (Eighteenth Annual, 1932)------ 10
444 Wind-Tunnel Research Comparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. VI-Skewed Ailerons on Rectangu-
lar Wings. By Fred E. Weick and Thomas
A. Harris. (Nineteenth Annual, 1933)------ .05
445 Working Charts for the Determination of the
Lift Distribution between Biplane Wings.
By Paul Kuhn. (Nineteenth Annual, 1933)--_ 10
456 The Aerodynamic Forces and Moments Exerted
on a Spinning Model of the "NY-1" Airplane
as Measured by the Spinning Balance. By
M. J. Bamber and C. H. Zimmerman. (Nine-
teenth Annual, 1933)---------------------- .05
462 Tests of Nacelle-Propeller Combinations in
Various Positions with Reference to Wings.
Part III-Clark Y Wing-Various Radial-
Engine Cowlings-Tractor Propeller. By
Donald H. Wood. (Nineteenth Annual,
1933) -----------------------------------. 10
468 The Interference between Struts in Various Com-
binations. By David Biermann and William
H. Herrnstein, Jr. (Nineteenth Annual, 1933) .05
472 Wind-Tunnel Tests on Combinations of a Wing
with Fixed Auxiliary Airfoils having Various
I Chords and Profiles. By Fred E. Weick and
Robert Sanders. (Nineteenth Annual. 1933)) .10










AIRPLANES-MODEL EXPERIMENTS-Continued

No. Title Price

499 Wind-Tunnel Research Comparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. XII-Upper-Surface Ailerons on
Wings with Split Flaps. By Fred E. Weick
and Carl J. Wenzinger. (Twentieth Annual,
1934) ---------------------------------$0. 10
505 Tests of Nacelle-Propeller Combinations in
Various Positions with Reference to Wings.
IV-Thick Wing-Variotfs Radial-Engine
Cowlings-Tandemin Propellers. By James G.
McHugh. (Twentieth Annual, 1934)-------- 15
506 Tests of Nacelle-Propller Combinations in
Various Positions with Reference to Wings.
V-Clark Y Biplane Cellule-N. A. C. A.
Cowled Nacelle-Tractor Propeller. By E.
Floyd Valentine. (Twentieth Annual, 1934)_ 10
507 Tests of Nacelle-Propeller Combinations in
Various Positions with Reference to Wings.
VI-Wings and Nacelles with Pusher Pro-
peller. By Donald H. Wood and Carlton
Bioletti. (Twentieth Annual, 1934) --------- 10
510 Wind-Tunnel Research Comparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. XIII-Auxiliary Airfoils Used as
External Ailerons. By Fred E. Weick and
Richard W. Noyes. (Twenty-First Annual,
1935)----------------------------------. 10
519 Spinning Characteristics of Wings. I-Rec-
tangular Clark Y Monoplane Wing. By M.
J. Bamber and C. H. Zimmerman. (Twenty-
First Annual, 1935).------------------- 10
528 Reduction of Hinge Moments of Airplane Con-
trol Surfaces by Tabs. By Thomas A. Harris.
(Twenty-First Annual, 1935)--------------- 10
540 Interference of Wing and Fuselage from Tests
of 209 Combinations in the N. A. C. A. Vari-
able-Density Tunnel. By Eastman N. Ja-
cobs and Kenneth E. Ward. (Twenty-First
Annual, 1935)--..------..------------- 10








21

AIRPLANES-MODEL EXPERIMENTS-Continued

No. Title Price

549 Wind-Tunnel Investigation of the Aerodynamic
Balancing of Upper-Surface Ailerons and Split
Flaps. By Carl J. Wenzinger. (Twenty-
Second Annual, 1936)----------------------------

AIRSHIPS

'115 Bending Moments, Envelope and Cable Stresses
in Nonrigid Airships. By C. P. Burgess.
(Seventh Annual, 1921)--------------------------
117 The Drag of Zeppelin Airships. By Max M.
Munk. (Seventh Annual, 1921)------------ $0.05
138 The Drag of "C" Class Airship Hull with Vary-
ing Lengths of Cylindric Midships. By A. F.
Zahm, R. H. Smith. and G. C. Hill. (Eighth
Annual, 1922)---------------------------- .05
164 The Inertia Coefficients of an Airship in a Fric-
tionless Fluid. By H. Bateman. (Ninth
Annual, 1923)---------------------------- .05
184 The Aerodynamic Forces on Airship Hulls. By
Max M. Munk. (Ninth Annual, 1923)------------
204 Forces on Airships in Gusts. By C. P. Burgess.
(Tenth Annual, 1924)---------------------- .05
208 Determination of the Turning Characteristics of
an Airship by Means of a Camera Obscura.
By J. W. Crowley, jr., and R. G. Freeman.
(Tenth Annual, 1924)---------------------- 10
210 Inertia Factors of Ellipsoids for Use in Airship
Design. By L. B. Tuckerman. (Eleventh
Annual, 1925)---------------------------- .05
211 Water Model Tests for Semirigid Airships. By
L. B. Tuckerman. (Eleventh Annual, 1925) - .05
212 Stability Equations for Airship Hulls. By A. F.
Zahm. (Eleventh Annual, 1925)----------- .05
215 Air Forces, Moments, and Damping on Model
of Fleet Airship Shenandoah. By A. F.
Zahm, R. H. Smith, and F. A. Louden.
(Eleventh Annual, 1925) -------------------. 15
Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










AlIRSHIPS- Continued


No. Title Price

223 Pressure Distribution on the C-7 Airship. By
J. W. Crowley, jr., and S. J. DeFrance.
(Eleventh Annual, 1925)------------------- $0. 15
291 Drag of C-Class Airship Hulls of Various Fine-
ness Ratios. By A. F. Zahm, R. H. Smith,
andF.A.Louden. (Fourteenth Annual, 1928). 10
318S Speed and Deceleration Trials of U. S. S. Los
Angeles, September, 1927. By S. J. DeFrance
and C. P. Burgess. (Fifteenth Annual, 1929)- .10
324 Flight Tests on U. S. S. Los Angeles. Part I.
FuU-Scale Pressure Distribution Investigation.
By S. J. DeFrance. (Fifteenth Annual, 1929)_ .15
325 Flight Tests on U. S. S. Los Angeles. Part II.
Stress and Strength Determination. By C.
P. Burgess. (Fifteenth Annual, 1929)----- 15
333 Full-Scale Turning Characteristics of the U.S.S.
Los Angeles. By F.L.Thompson. (Fifteenth
Annual, 1929) ---------------------------- 10
394 Airship Model Tests in the Variable Density
Wind Tunnel. By Ira H. Abbott. (Seven-
teenth Annual, 1931)--------------------- .20
397 The Drag Characteristics of Several Airships
Determined by Deceleration Tests. By F. L.
Thompson and H. W. Kirschbaum. (Seven-
teenth Annual, 1931) ------------------ 10
405 Application of Practical Hydrodynamics to Air-
ship Design. By R. H. Upson and W. A.
Klikoff. (Eighteenth Annual, 1932) _------ 15
430 Measurements of Flow in the Boundary Layer
a 1/40-Scale Model of the U. S. Airship
"Akron." By Hugh B. Freeman. (Eight-
eenth Annual, 1932)----------------------- .05
432 Force Measurements on a 1/40-Scale Model of
the U. S. Airship "Akron." By Hugh B.
Freeman. (Eighteenth Annual, 1932) ------ .05
443 Pressure-Distribution Measurements on the
Hull and Fins of a 1/40-Scale Model of the
U. S. Airship "Akron." By Hugh B. Free-
man. (Nineteenth Annual, 1933)--------' .05
451 The Drag of Two Streamline Bodies as Affected
bv Protuberances and Appendages. By Ira
H. Abbott. (Nineteenth Annual, 1933)------ .05










ENGINES AND ACCESSORIES

No. Title Price

1 7 Thermodynamic Efficiency of Present Types of
Internal Combustion Engines for Aircraft.
By Columbia University. (First Annual, 1915) ------
Part 1. Review of the Development of
Engines Suitable for Aeronautic Service.
Part 2. Aero Engines Analyzed with Refer-
ence to Elements of Process or Function.
S10 Mufflers for Aeronautic Engine. By H. Die-
derichs and G. B. Upton. (Second Annual,
1916)----------------------------------------
11 Carburetor Design-A Preliminary Study of the
State of the Art. By Charles Edward Lucke,
assisted by Friedrich Otto Willhofft. (Sec-
ond Annual, 1916)------------------------------
1 23 Aeronautic Power-Plant Investigations. By the
Subcommittee on Power Plants. (Third
Annual, 1917)----------------------------------
Part 1. Performance of Aeronautic Engines
at High Altitudes.
Part 2. Radiator Design.
Part 3. Spark Plugs.
3 24 Air Flow through Poppet Valves. By G. W.
Lewis and E. M. Nutting. (Fourth Annual,
1918)--------------------------------------
343 Synopsis of Aeronautic Radiator Investigations
for the years 1917 and 1918. By R. V. Klein-
schmidt. (Fourth Annual. 1918)----------------
345 Effect of Compression Ratio, Pressure, Tem-
perature, and Humidity on Power. (Fourth
Annual, 1918)----------------------------------
Part 1. Variation of Horsepower with Al-
titude and Compression Ratio. By
H. C. Dickinson, W. S. James, and G.,V.
Anderson.
Part 2. Value of Supercharging. By H. C.
Dickinson and G. V. Anderson.
I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
I Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.








24

ENGINES AND ACCESSORIES-Continued


Title


Price


No.

345






46
348


'49

351






52

3 53


SOut of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and In
the libraries of large cities.
SOut of Print. Available as a separate report for reference or loan In the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.


Effect of Compression Ratio, Pressure, Tern-
perature and Humidity on Power. (Fourth
Annual, 1918)-Continued.
Part 3. Variation of Horsepower with
Temperature. By H. C. Dickinson,
W. S. James, and G. V. Anderson.
Part 4. Influence of Water Injection on En-
gine Performance. By V. W. Brinkerhoff.
A Study of Airplane Engine Tests. By V. R.
Gage. (Fourth Annual 1918)--------------------
Carbureting Conditions Characteristic of Air-
craft Engines. By P. S. Tice. (Fourth
Annual, 1918)--- --------------------------
Metering Characteristics of Carburetors. By
P. S. Tice. (Fourth Annual, 1918)---------------
Spark-Plug Defects and Tests. (Fifth Annual,
1919)
Part 1. Causes of Failure of Spark Plugs.
By F. B. Silsbee.
Part 2. Gas Leakage in Spark Plugs. By
L. Sawyer.
Part 3. Methods for Tests of Spark Plugs.
By H. C. Dickinson.
Temperatures in Spark Plugs having Steel and
Brass Shells. By C. S. Cragoe. (Fifth Annual,
1919)--------------------------------- $0.05
Properties and Preparation of Ceramic Insula-
tors for Spark Plugs. (Fifth Annual, 1919)---------
Part 1. Methods of Measuring Resistance
of Insulators at High Temperatures.
By F. B. Silsbee and R. K. Honaman.
Part 2. Electrical Resistance of Various In-
sulating Materials at High Temperatures.
By R. K. Honaman and E. L. Fonseca.
Part 3. Preparation and Composition of
Ceramic Bodies for Spark-Plug Insula-
tors. By A. V. Bleininger.
Part 4. Cements for Spark-PlugElectrodes.
Bv H. F. Stalev.










ENGINES AND ACCESSORIES-Continued

No. Title Price

54 Effect of Temperature and Pressure on the
Sparking Voltage. By F. B. Silsbee and L.
B. Loeb. (Fifth Annual, 1919) -----------------
55 Investigation of the Muffling Problem for Air-
plane Engines. By G. B. Upton and V. R.
Gage. (Fifth Annual, 1919)--------------- $0. 10
S56 Heat Energy of Various Ignition Sparks. (Fifth
Annual, 1919)---------------------------------
Part 1. Method of Measuring Heat Energy
of Ignition Sparks. By F. B. Silsbee, L.
B. Loeb, and E. L. Fonseca.
Part 2. Measurement of Heat Energy per
Spark of Various Ignition Systems. By'
F. B. Silsbee and E. L. Fonseca.
3 57 The Subsidiary Gap as a Means for Improving
Ignition. By W. S. Gorton. (Fifth Annual,
1919)-----------------------------
58 Characteristics of High-Tension Magnetos.
(Fifth Annual. 1919)----------------------------
Part 1. Cycle of Operation of Jump-Spark
Ignition Systems. By F. B. Silsbee.
Part 2. Transformation Ratio and Coupling
in High-Tension Magnetos. By F. B.
I Silsbee.
59 General Analysis of Airplane Radiator Problems.
By H. C. Dickinson, W. S. James, and R. V.
Kleinschmnidt. (Fifth Annual, 1919)--------- .05
60 General Discussion of Test Methods for Radi-
ators. By H. C. Dickinson, W. S. James, and
W. B. Brown. (Fifth Annual, 1919)-------- 10
61 Head Resistance Due to Radiators. (Fifth
Annual, 1919)--------------------------- .10
Part 1. Head Resistance of Radiator Cores.
By R. V. Kleinschmidt and S. R. Parsons.
Part 2. Preliminary Report on Resistance
Due to Nose Radiator. By R. V. Klein-
I schmidt.
Part 3. Effect of Streamline Casing for
Free Air Radiators. By S. R. Parsons.
SOut of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.








26


ENGINES AND ACCESSORIES-Continued

No. Title Price

62 Effect of Altitude on Radiator Performance.
By W. S. James and S. R. Parsons. (Fifth
Annual, 1919)-------------------------- $0.10
63 Results of Tests on Radiators for Aircraft En-
gines. (Fifth Annual, 1919) ----------------. 10
Part 1. Heat Dissipation of Radiators. By
H. C. Dickinson, W. S. James, and R. V.
Kleinschmidt.
Part 2. Water Flow through Radiator
Cores. By W. S. James.
186 Properties of Special Types of Radiators. By
S. R. Parsons. (Sixth Annual, 1920) -------------
8 87 Effects of Nature of Cooling Surface on Radiator
Performance. By S. R. Parsons and R. V.
Kleinschmidt. (Sixth Annual, 1920) -----------
88 Pressure Drop in Radiator Air Tubes. By S. R.
Parsons. (Sixth Annual, 1920)--- ------ .05
101 The Calculated Performance of Airplanes
Equipped with Supercharging Engines. By
E. C. Kemble. (Sixth Annual, 1920)--------------
102 Performance of a Liberty 12 Airplane Engine.
By S. W. Sparrow and H. S. White. (Sixth
Annual, 1920)-------------------------------
S103 Performance of a 300-horsepower Hispano-
Suiza Airplane Engine. By S. W. Sparrow
and H. S. White. (Sixth Annual, 1920) -----------
106 Turbulence in the Air Tubes of Radiators for
Aircraft Engines. By S. R. Parsons. (Sixth
Annual. 1920).------------------- .05
S108 Some Factors of Airplane Engine Performance.
By Victor R. Gage. (Sixth Annual, 1920) --- ------
1123 Simplified Theory of the Magneto. By F. B.
Silsbee. (Seventh Annual, 1921) -----
134 Performance of Maybach 300-horsepower Air-
plane Engine. By S. W. Sparrow. (Eighth
Annual, 1922)--..----------------------------
'135 Performance of B. M. W. 185-horsepower Air-
plane Engine. By S. W. Sparrow. (Eighth
Annual, 1922)-.----- -------------- ------
I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the Ulbrariea of large cities.
I Out of print. Available as a separate report for reference or loan In the OfMe
of Aeronautical Intelligence. National Advisory Committee for Aeronautics.








27


ENGINES AND ACCESSORIES-Continued


No.

3 158


Ss 159

4 171

3 179


: '187
I,
3: 189

I s 190

v 202

205

222

224

S230


3 239


Title


Price


Mathematical Equations for Head Conduction
in the Fins of Air-Cooled Engines. By D. R.
Harper and W. G. Brown. (Eighth Annual,
1922)------------------------------------------
Jet Propulsion for Airplanes. By Edgar Buck-
ingham. (Ninth Annual, 1923)-------------------
Engine Performance and the Determination of
Absolute Ceiling. By Walter S. Diehl.
(Ninth Annual, 1923)---------------------------
The Effect of Electrode Temperature on the
Sparking Voltage of Short Spark Gaps. By
F. B. Silsbee. (Ninth Annual, 1923)--------
Flame Speed and Spark Intensity. By D. W.
Randolph and F. B. Silsbee. (Tenth Annual,
1924)------------------------------------------
Relation of Fuel-Air Ratio to Engine Perform-
ance. By Stanwood W. Sparrow. (Tenth
Annual, 1924)--------------------------------
Correcting Horsepower Measurements to a
Standard Temperature. By Stanwood W.
Sparrow. (Tenth Annual, 1924)------------------
The Sparking Voltage of Spark Plugs. By F. B.
Silsbee. (Tenth Annual, 1924)------------- $0. 05
The Effect of Changes in Compression Ratio
upon Engine Performance. By Stanwood
W. Sparrow. (Tenth Annual, 1924)-------- 10
Spray Penetration with a Simple Fuel Injection
Nozzle. By Harold E. Miller and Edward G.
Beardsley. (Eleventh Annual, 1925)-------- 05
An Investigation of the Coefficient of Discharge
of Liquids through Small Round Orifices.
By W. F. Joachim. (Eleventh Annual, 1925)_ .05
Description and Laboratory Tests of a Roots
Type Aircraft Engine Supercharger. By
Marsden Ware. (Eleventh Annual, 1925)--- - --
Power Output and Air Requirements of a Two-
Stroke Cycle Engine for Aeronautical Use.
By C. R. Paton and Carlton Kemper.
(Twelfth Annual, 1926)--------------------------


* Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence. National Advisory Committee for Aeronautics.
27903-36-----3










ENGINES AND ACCESSORIES-Continued

No. Title Price

241 Electrical Characteristics of Spark Generators I
for Automotive Ignition. By R. B. Brode,
D. W. Randolph, and F. B. Silsbee. (Twelfth
Annual, 1926)-------------------------- $0.15
243 A Preliminary Study of Fuel Injection and Com-
pression Ignition as Applied to an Aircraft
Engine Cylinder. By Arthur W. Gardiner.
(Twelfth Annual, 1926)-------------------- .10
250 Description of the N. A. C. A. Universal Test
Engine and some Test Results. By Marsden
Ware. (Twelfth Annual, 1926)------------- 10
252 The Direct Measurement of Engine Power on an
Airplane in Flight with a Hub Type Dyna-
mometer. By W. D. Gove and M. W. Green.
(Twelfth Annual, 1926)------------------ .10
258 Some Factors Affecting the Reproducibility of
Penetration and the Cut-Off of Oil Sprays for
Fuel Injection Engines. By E. G. Beardsley.
(Thirteenth Annual, 1927)-- --------------. 05
3 261 Resistance and Cooling Power of Various Radia-
tors. By R. H. Smith. (Thirteenth Annual,
1927) -------------------------------
262 Friction of Aviation Engines. By S. W. Spar-
row and M. A. Thorne. (Thirteenth Annual,
1927)-------------------------------- .10
263 Preliminary Flight Tests of the N. A. C. A.
Roots Type Aircraft Engine Supercharger.
By Arthur W. Gardiner and Elliott G. Reid.
(Thirteenth Annual, 1927)----------------- 10
268 Factors in the Design of Centrifugal Type In-
jection Valves for Oil Engines. By W. F.
Joachim and E. G. Beardsley. (Thirteenth
Annual, 1927)------------------------. .10
272 The Relative Performance Obtained with Several
Methods of Control of an Overcompressed
Engine Using Gasoline. By Arthur W. Gar-
diner and William E. Whedon. (Thirteenth I
Annual, 1927)------ ----------- 10
I Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










ENGINES AND ACCESSORIES-Continued

No. Title Price

274 The N. A. C. A. Photographic Apparatus for
Studying Fuel Sprays from Oil Engine Injec-
tion Valves and Test Results from Several
Researches. By Edward G. Beardsley.
(Thirteenth Annual, 1927)----------------- $0.10
276 Combustion Time in the Engine Cylinder and
Its Effect on Engine Performance. By
Charles F. Marvin, jr. (Thirteenth Annual,
1927)----------------------------------- .10
277 The Comparative Performance of an Aviation
Engine at Normal and High Inlet Air Tem-
peratures. By Arthur W. Gardiner and Oscar
W. Schey. (Thirteenth Annual, 1927)------ .10
281 The Effects of Fuel and Cylinder Gas Densities
on the Characteristics of Fuel Sprays for Oil
Engines. By W. F. Joachim and Edward G.
Beardsley. (Thirteenth Annual, 1927)------ .10
3 282 The Performance of Several Combustion Cham-
bers Designed for Aircraft Oil Engines. By
William F. Joachim and Carlton Kemper.
(Thirteenth Annual, 1927)--------- -
283 A Preliminary Investigation of Supercharging an
Air-Cooled Engine in Flight. By Marsden
Ware and Oscar W. Schey. (Fourteenth
Annual, 1928)----------------------- .10
284 The Comparative Performance of Roots Type
Aircraft Engine Superchargers as Affected by
Change in Impeller Speed and Displacement.
By Marsden Ware and Ernest E. Wilson.
(Fourteenth Annual, 1928)---.---------. 10
294 The Measurement of Maximum Cylinder Pres-
sures. By Chester W. Hicks. (Fourteenth
Annual, 1928)---------------------------- .15
295 The Variation in Engine Power with Altitude
Determined from Measurements with a Hub
Dynamometer. By W. D. Gove. (Four-
teenth Annual, 1928)---------------------- .10
i Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics.










ENGINES AND ACCESSORIES-Continued

No. Title Price

303 An Investigation of the Use of Discharge Valves
and an Intake Control for Improving the Per-
formance of N. A. C. A. Roots Type Super-
Scharger. By Oscar W. Schey and Ernest E.
Wilson. (Fourteenth Annual, 1928)____ $0. 10
313 Drag and Cooling with Various Forms of Cowl-
ing for a "Whirlwind" Radial Air-Cooled
Engine-I. By Fred E. Weick. (Fifteenth
Annual, 1929)---------------------------- 15
314 Drag and Cooling with Various Forms of Cowl-
ing for a "Whirlwind" Radial Air-Cooled
Engine-IT. By Fred E. Weick. (Fifteenth
SAnnual, 1929)---------------------------- .20
327 The Effect of Supercharger Capacity on Engine
and Airplane Performance. By C. W. Schey
and W. D. Gove. (Fifteenth Annual, 1929).--i .10
330 Experimental and Analytical Determination of
the Motion of Hydraulically Operated Valve
Stems in Oil Engine Injection Systems. By
A. G. Gellales and A. M. Rothrock. (Fifteenth
Annual, 1929)------------------------- 10
332 The Effect of Cowling on Cylinder Tempera-
tures and Performance of a Wright J-5 En-
gine. By Oscar W. Schey and Arnold E.
Biermann. (Fifteenth Annual, 1929)------- 15
341 The Design and Development of an Automatic
Injection Valve with an Annular Orifice of
Varying Area. By William F. Joachim,
Chester W. Hicks and Hampton W. Foster.
(Sixteenth Annual, 1930)---------------. 10
355 Comparative Flight Performance with an N. A.
C. A. Roots Supercharger and a Turbocen-
trifugal Supercharger. By Oscar W. Schey
and Alfred W. Young. (Sixteenth Annual,
1930)------------------------------------ .10
359 An Investigation of the Effectiveness of Ignition
Sparks. By Melville F. Peters, Wayne L.
Summervillc, and Merlin Davis. (Sixteenth
Annual, 19:i0)--------------------------- 10
30: Pressure Fluctuation in a Common-Rail Fuel
Injection System. By A. M. Rothrock.
(Sixteenth Annual, 1930)------------------- 10








31

ENGINES AND ACCESSORIES-Continued

No. Title Price

373 Coefficients of Discharge of Fuel Injection Noz-
zles for Compression-Ignition Engines. By
A. G. Gelalles. (Seventeenth Annual, 1931)__ $0. 10
374 The Automotive Ignition Coil. By T. H. Dar-
nell. Note by F. B. Silsbee. (Seventeenth
Annual, 1931) ---------------------------- .25
384 The Comparative Performance of Superchargers.
By Oscar W. bchey (Seventeenth Annual,
1931) ------------------------------------- .05
390 The Effect of Valve Timing upon the Perform-
ance of a Supercharged Engine at Altitude and
an Unsupercharged Engine at Sea Level. By
Oscar W. Schey and Arnold E. Biermann.
S(Seventeenth Annual, 1931)---------------- 10
396 Hydraulics of Fuel Injection Pumps for Comn-
pression-Ignition Engines. By A. M. Roth-
rock. (Seventeenth Annual, 1931)---------- .25
399 Flame Movement and Pressure Development in I
an Engine Cylinder. By Charles F. Marvin
and Robert D. Best. (Seventeenth Annual,
1931)------------------------------------ 10
401 Combustion in High-Speed Compression-Igni-
tion Engine. By A. M. Rothrock. (Eight-
eenth Annual, 1932)----------------------- 15
402 Effect of Orifice Length-Diameter Ratio on Fuel
Sprays for Compression-Ignition Engine. By
A. G. Gelalles. (Eighteenth Annual, 1932) - .15
403 Ice Prevention on Aircraft by Means of Engine i
Exhaust Heat and a Technical Study of Heat
Transmission from a Clark Y Airfoil. By
Theodore Theodorsen & William C. Clay.
(Eighteenth Annual, 1932)------------------- .20
404 The Effect of Increased Carburetor Pressure on
Engine Performance at Several Compression
Ratios. By Oscar W. Schey and Vern G.
Rollin. (Eighteenth Annual, 1932)-------- 10
409 The Elimination of Fire Hazard due to Back-
Fires. Theodore Theodorsen and Ira M.
Freeman. (Eighteenth Annual, 1932)-------- 10
414 The Effect on Airplane Performance of Several
Types of Low-Drag Cowling for Radial Air-
Cooled Engines. By Win. H. McAvoy,
Oscar W. Schey, and Alfred W. Young.
S(Eighteenth Annual, 1932) -------------------.20










ENGINES AND ACCESSORIES-Continued

No. Title Price

425 The Effect of Nozzle Design and Operation Con-
ditions on the Atomization and Distribution
of Fuel Sprays. By Dana W. Lee. (Eight-
eenth Annual, 1932)---------------------- $0.10
426 The Effect of Humidity on Engine Power at
Altitude. By D. B. Brooks and E. A. Gar-
lock. (Eighteenth Annual, 1932)----------- .05
429 The N. A. C. A. Apparatus for Studying the For-
mation and Combustion of Fuel Sprays and
the Results from Preliminary Tests. Bv
A. M. Rothrock. (Eighteenth Annual, 1932)_. 10
433 Rates of Fuel Discharge as Affected by the De-
sign of Fuel-Injection Systems for Internal-
Combustion Engines. Bv A. G. Gelalles and
E. T. Marsh. (Eighteenth Annual, 1932)- 05
435 Fuel Vaporization and its Effect on Combustion
in a High-Speed Compression-Ignition Engine.
By A. M. Rothrock and C. D. Waldron.
(Eighteenth Annual, 1932)----------------- 10
438 Experiments on the Distribution of Fuel in Fuel
Spray s. By Dana W. Lee. (Eighteenth An-
nual, 1932)------------------------------ 10
440 The Mechanism of Atomization Accompanying
Solid Injection. By R. A. Castleman, Jr.
(Eighteenth Annual, 1932)----------------- .05
454 Photomicrographic Studies of Fuel Sprays. By
Dana W. Lee and Robert C. Spencer. kNine-
teenth Annual, 1933)---------------------- 10
455 Penetration and Duration of Fuel Sprays from a
Pump Injection System. Bv A. M. Rothrock
and E. T. Marsh. (Nineteenth Annual, 1933) .05
469 Increasing the Air Charge and Scavenging the
Clearance Volume of a Compression-Ignition
Engine. By J. A. Spanogle, C. W. Hicks, and
H. H. Foster. (Nineteenth Annual, 1933) --- 05
471 Performance of a Fuel-Injection Spark-Ignition
Engine Using a Hydrogenated Safety Fuel.
By Oscar W. Schey and Alfred W. Young.
(Nineteenth Annual, 1933)----------------- .05










ENGINES AND ACCESSORIES-Continued

No. Title Price

477 Effect of Viscosity on Fuel Leakage between
Lapped Plungers and Sleeves and on the Dis-
charge from a Pump-Injection System. By
A. M. Rothrock and E. T. Marsh. (Twentieth
Annual, 1934)---------------------------- $0. 10
483 Effect of Moderate Air Flow on the Distribution
of Fuel Sprays after Injection Cut-Off. By
A. M. Rothrock and R. C. Spencer. (Twen-
tieth Annual, 1934)------------------------ .10
486 Infrared Radiation from Explosions in a Spark-
Ignition Engine. By Charles F. Marvin,
Jr., Frank R. Caldwell, and Sydney Steele.
(Twentieth Annual, 1934) ------------------ 10
488 Heat Transfer from Finned Metal Cylinders in
an Air Stream. By Arnold E. Biermann and
Benjamin Pinkel. (Twentieth Annual, 1934). .10
493 The Physical Effects of Detonation in a Closed
Cylindrical Chamber. By C. S. Draper.
(Twentieth Annual, 1934) ------------------ 10
495 A Description and Test Results of a Spark-
Ignition and a Compression-Ignition 2-Stroke-
Cycle Engine. By J. A. Spanogle and E. G.
Whitney. (Twentieth Annual, 1934)-------- .10
511 The Effect of Baffles on the Temperature Dis-
tribution and Heat-Transfer Coefficients of
Finned Cylinders. By Oscar W. Schey and
Vern G. Rollin. (Twenty-First Annual,
1935)------------ ------------. 10
512 Some Factors Affecting Combustion in an Inter-
I nal-Combustion Engine. By A. M. Rothrock
and Mildred Cohn. (Twenty-First Annual,
1935)----------------------------------- 10
520 A Comparison of Fuel Sprays from Several
Types of Injection Nozzles. By Dana W.
Lee. (Twenty-First Annual, 1935)---------- .25
525 Some Effects of Injection Advance Angle, Engine-
Jacket Temperature, and Speed on Combus-
tion in a Compression-Ignition Engine. By
A. M. Rothrock and C. D. Waldron. (Twen-
ty-First Annual, 1935)---------------------. 10




*:i




34

ENGINES AND ACCESSORIES-Continued

No. Title Price

533 Distribution and Regularity of Injection from a
Multicylinder Fuel-Injection Pump. By A.
M. Rothrock and E. T. Marsh. (Twenty-
First Annual, 1935)------------------------ $0. 10
544 Combustion in a Bomb with a Fuel-Injection
System. By Mildred Cohn and R. C. Spen-
cer. (Twenty-Second Annual, 1936) --------------
545 Effects of Air-Fuel Ratio on Fuel Spray and
Flame Formation in a Compression-Ignition
Engine. By A. M. Rothrock and C. D. Wal-
dron. (Twenty-Second Annual, 1936)-------------
550 Cooling Characteristics of a 2-Row Radial
Engine. By Oscar W. Schey and Vern G.
Rollin. (Twenty-Second Annual, 1936)-----------

FUELS

3 42 A New Process for the Production of Aircraft-
Engine Fuels. By Auguste Jean Paris, jr.,and
W. Francklyn Paris. (Fourth Annual, 1918)-------
347 Power Characteristics of Fuels for Aircraft
Engines. (Fourth Annual, 1918)------------------
Part 1. Power Characteristics of Aviation
Gasoline. By E. W. Roberts.
Part 2. Power Characteristics of Sumatra
and Borneo Gasolines. By E. W. Roberts.
Part 3. Power Characteristics of 20 per
cent Benzol Mixtures. By E. W. Roberts.
89 Comparison of Alcogas Aviation Fuel with
Export Aviation Gasoline. By V. R. Gage,
S. W. Sparrow, and D. R. Harper. (Sixth
Annual, 1920)---------------------------- $0.05
90 Comparison of Hector Fuel with Export Aviation
Gasoline. By H. C. Dickinson, V. R. Gage,
and S. W. Sparrow. (Sixth Annual, 1920)_... 05
232 Fuels for 11igh-Compression Engines. By Stan-
wood W. Sparrow. (Eleventh Annual, 1925) 10
280 The Gaseous Explosive Reaction-The Effect of
Inert Gases. By F. W. Stevens. (Thirteenth
Annual, 1927)-------------------------I 10
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronnul ical Intelligenice, National Advisory Committee for Aeronautics.








35

FUELS-Continued


No. Title Price

305 The Gaseous Explosive Reaction-A Study of
the Kinetics of Composite Fuels. By F. W.
Stevens. (Fourteenth Annual, 1928)-------- $0. 15
321 Fuel Vapor Pressures and Their Relation to the
Preparation of Fuel for Combustion in Fuel
Injection Engines. By W. F. Joachim and
A. M. Rothrock. (Fifteenth Annual, 1929)- .... - 10
337 The Gaseous Explosive Reaction at Constant
SPressure-The Reaction Order and Reaction
Rate. By F. W. Stevens. (Sixteenth Annual,
1930) ---------------------------------- 10
372 The Gaseous Explosive Reaction: The Effect of
Pressure on the Rate of Propagation of the
Reaction Zone and upon the Rate of Molecular
Transformation, By F. W. Stevens. (Seven-
teenth Annual, 1931)---------------------- .15
476 Relation of Hydrogen and Methane to Carbon
Monoxide in Exhaust Gases from Internal-
Combustion Engines. By Harold C. Gerrish
and Arthur M. Tessmann. (Twentieth An-
nual, 1934)------------------------------- .05
531 The Effect of Water Vapor on Flame Velocity
in Equivalent CO-02 Mixtures. By Ernest
F. Fiock and H. Kendall King. (Twenty-
First Annual, 1935)------------------------ .05
532 The Soap-Bubble Method of Studying the Com-
bustion of Mixtures of CO and 02. By Ernest
F. Fiock and Carl H. Roeder. (Twenty-
First Annual, 1935)------------------------ .05
535 Hydrogen as an Auxiliary Fuel in Compression-
Ignition Engines. By Harold C. Gerrish and
Hampton H. Foster. (Twenty-First Annual,
1935) ----------------------------------- 10


GASES

40 The Ferrosilicon Process for the Generation of
Hydrogen. By E. R. Weaver, W. M. Berry,
V. L. Bohnson, and B. D. Gordon. (Fourth
Annual, 1918)----------------------------
41 Testing of Balloon Gas. By Junius David
Edwards. (Fourth Annual, 1918) -----------


$0. 15


. 05


I








36
HELICOPTERS

No. Title Price

3 SO Stability of the Parachute and Helicopter. By
H. Bateman. (Fifth Annual, 1919)---------------

HYDRODYNAMICS

116 Applications of Modern Hydrodynamics to
Aeronautics. By L. Prandtl. (Seventh
Annual, 1921) -------------------------$0. 10
405 Application of Practical Hydrodynamics to Air-
ship Design. By R. H. Upson and W. A.
SKlikoff. (Eighteenth Annual, 1932) --------- .15
470 The N. A. C. A. Tank-A High-Speed Towing
Basin for Testing Models of Seaplane Floats.
Bv Starr Truscott. (Nineteenth Annual,
1933)------------------------------------ 10
503 The Effect of Spray Strips on the Take-Off Per-
formance of a Model of a Flying-Boat Hull.
By Starr Truscott. (Twentieth Annual, 1934)-, 10
543 Tank Tests of N. A. C. A. Model 40 Series of
Hulls for Small Flying Boats and Amphibians.
By John B. Parkinson and John R. Dawson. ,
(Twenty-Second Annual, 1936) --------------------

INSTRUMENTS

1 2 Investigation of Pitot Tubes. (First Annual,
1915)------------------------------------------
Part 1. The Pitot Tube and Other Ane-
mometers for Airplanes. By W. H.
Herschel.
Part 2. The Theory of the Pitot and Ven-
turi Tubes. By E. Buckingham.
1 8 General Specifications Covering Requirements
of Aeronautic Instruments. By National
Advisory Committee for Aeronautics. (Sec-
ond Annual, 1916)-----------------------------
31 Development of Air Speed Nozzles. By A. F.
Zahm. (Fourth Annual, 1918)------------- $0. 10
I Out or print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities
8 Out of print. Available as a separate report for reference or loan in the Offmoe
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










INST RUMENTS-Continued

No. Title Price

32 The Airplane Tensiometer. By L. J. Larson.
(Fourth Annual, 1918)-------------------- $0.05
50 Calculation of Low Pressure Indicator Dia-
grams. By E. C. Kemble. (Fourth Annual,
1918)------------------------------------ .05
81 Comparison of U. S. and British Standard
Pitot-Static Tubes. By A. F. Zahm and R. H.
Smith! (Fifth Annual, 1919)--------------- .05
94 The Efficiency of Small Bearings in Instruments
of the Type Used in Aircraft. By F. H.
Norton. (Sixth Annual, 1920) ..- ---------- .05
99 Acceleration in Flight. By F. H. Norton and
E. T. Alien. (Sixth Annual, 1920)--------. .10
3100 Accelerometer Design. By F. H. Norton and
Edward P. Warner. (Sixth Annual, 1920) ---------
3 107 A High-Speed Engine Pressure Indicator of the
Balanced Diaphragm Type. By H. C. Dick-
inson and F. B. Newell. (Sixth Annual, 1920) -------
3 110 The Altitude Effect on Air Speed Indicators.
By M. D. Hersey, F. L. Hunt, and H. N.
Eaton. (Sixth Annual, 1920)--------------------
125 Aeronautic Instruments: Section I-General
Classification of Instruments and Problems,
Including Bibliography. By Bureau of
Standards. (Seventh Annual, 1921) --------- .05
126 Aeronautic Instruments: Section II-Altitude
Instruments. By Bureau of Standards.
(Seventh Annual, 1921)-------------------- .25
Part 1. Altimeters and Barographs.
Part 2. Precision Altimeter Design.
Part 3. Statiscopes and Rate-of-Climb In-
dicators.
Part. 4. Aerographs and Strut Thermome-
ters.
127 Aeronautic Instruments: Section III-Aircraft
Speed Instruments. By Bureau of Stand-
ards. (Seventh Annual, 1921)-------------- 10
Part 1. Air Speed Indicators.
Part 2. Testing of Air Speed Meters.
Part 3. Principles of Ground-Speed Instru-
ments.
I Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










INSTRUMENTS-Continued

No. Title Price

128 Aeronautic Instruments: Section IV-Direc-
tion Instruments. By Bureau of Standards.
(Seventh Annual, 1921)------------------ $0.25
Part 1. Inclinometers and Banking Indi-
cators.
Part 2. The Testing and Use of Magnetic
Compasses for Airplanes.
Part 3. Aircraft Compasses-Description
and Classification.
Part 4. Turn Indicators.
3129 Aeronautic Instruments; Section V-Power-
Plant Instruments. By Bureau of Stand-
ards. (Seventh Annual, 1921)--------------
Part 1. Airplane Tachometers.
Part 2. Testing of Airplane Tachometers.
Part 3. Thermometers for Aircraft Engines.
Part 4. Air-Pressure and Oil-Pressure
Gages.
Part 5. Gasoline-Depth Gages and Flow
Meters for Aircraft.
130 Aeronautic Instruments: Section VI-Oxygen
Instruments. By Bureau of Standards.
(Seventh Annual, 1921)-------------------- 10
131 Aeronautic Instruments: Section VII-Aerial
Navigation Instruments. By Bureau of
Standards. (Seventh Annual, 1921) --------- 10
132 Aeronautic Instruments: Section VIII-Recent
Developments and Outstanding Problems.
By Bureau of Standards. (Seventh Annual,
1921)------------------------------------ .05
3 156 The Altitude Effect of Air Speed Indicators-II.
By H. N. Eaton and W. A. McNair. (Eighth
Annual, 1922)---------------------------------
S160 An Airship Slide Rule. By E. R. Weaver and
S. F. Pickcring. (Ninth'Annual, 1923)------------
S165 Diaphragms for Aeronautic Instruments. By
M. D. Hcrsey. (Ninth Annual, 1923)-------------
,166 The Aerodynamic Plane Table. By A. F.
Zahm. (Ninth Annual, 1923)--------------------
SOuLi of print. Available as a sep:ir.ie reprwirt fur reference or loan in the Office
of Aeronautical Inlelligence, National Advi tury Committee for Aernnautics.






39

INSTRUMENTS-Continued

No. Title Price

3 176 A Constant-Pressure Bomb. By F. W. Stevens.
(Ninth Annual, 1923) ----------
198 Astronomical Methods in Aerial Navigation.
By K. Hilding Beij. (Tenth Annual, 1924)... $0. 15
199 Interference Tests on an N. A. C. A. Pitot Tube.
By Elliott G. Reid. (Tenth Annual, 1924)-- .05
3 206 Nonmetallic Diaphragms for Instruments. By
H. N. Eaton and C. T. Buckingham. (Tenth
Annual, 1924)---- ------------ ---
264 Differential Pressures on a Pitot-Venturi and a
Pitot-Static Nozzle over 360 Pitch and Yaw.
By R. M. Bear. (Thirteenth Annual, 1927)_2 .05
270 The Measurement of Pressure Through Tubes
in Pressure Distribution Tests. By Paul E.
Hemke. (Thirteenth Annual, 1927)------- .10
299 Investigation of Damping Liquids for Aircraft
Instruments. By G. H. Keulegan. (Four-
teenth Annual, 1928)---------------------- 10
310 Pressure Element of Constant Logarithmic
Stiffness for Temperature Compensated Alti-
meter. By W. G. Brombacher and F.
Cordero.. (Fifteenth Annual, 1929)------- -- 10
320 The Measurement of Fluctuations of Air Speed
by the Hot Wire Anemometer. By H. L.
Dryden and A. M. Keuthe. (Fifteenth An-
nual, 1929)------------------------------- 15
358 Temperature Coefficient of the Modulus of
Rigidity of Aircraft Instrument Diaphragm
and Spring Materials. By W. G. Brom-
bacher and E. R. Melton. (Sixteenth Annual,
1930)------------------------------------ .10
371 Present Status of Aircraft Instruments. By
the Subcommittee on Air Navigation In-
struments. (Seventeenth Annual, 1931)------ .15
388 Pressure Cell Investigation. By Theodore
Theodorsen. (Seventeenth Annual, 1931)---- .10
398 Investigation of Damping Liquids for Aircraft
Instruments-II. By M. R. Houseman and
G. H. Keulegan. (Seventeenth Annual, 1931)_ .15
Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence. National Advisory Committee for Aeronautics.








40


INSTRUMENTS-Continued


Title


420 Aircraft Speed Instruments. By K. Holding
Beij. (Eighteenth Annual, 1932)----------
448 Improved Apparatus for the Measurement of
Fluctuations of Air Speed in Turbulent Flow.
By W. C. Mock, jr.. and H. L. Dryden.
(Nineteenth Annual, 1933)-----------------
466 Aircraft Power-Plant Instruments. By Har-
court Sontag and W. G. Brombacher. (Nine-
teenth Annual, 1933)----------------------
513 Experimental Investigation of the Robinson-
Type Cup Anemometer. By M. J. Brevoort
and U. T. Joyner. (Twenty-First Annual,
1935)-------------------------------------
524 A Turbulence Indicator Utilizing the Diffusion of
Heat. By G. B. Schubauer. (Twenty-First
Annual, 1935)-----------------------------
551 Aircraft Compass Characteristics. By John B.
Peterson and Clyde W. Smith, U. S. N.
(Twenty-Second Annual, 1936)-------------


$0.10


.10


.15


.10

05

a
El
5,
.*


MATERIALS


15 Relative Worth of Improvements on Fabrics.
Bv the Goodyear Tire & Rubber Co.
(First Annual, 1915)----------------------- ------
1 6 Investigations of Balloon and Airplane Fabrics.,
(First Annual, 1915)-----------------------------
Part 1. Balloon and Airplane Fabrics. By
Willis A. Gibbons and Omar H. Smith. i
Part. 2. Skin Friction of Various Surfaces
in Air. By Willis A. Gibbons.
1 16 The Stretching of the Fabric and the Deforma-
tion of the Envelope in Nonrigid Balloons.
(Third Annual, 1917)--------------------------
Part 1. The Stretching of the Fabric and
the Shape of the Envelope. By Rudolf
Haas.
Part 2. The Deformation of the Envelope
of the Siemens-Schuckert Airships.
By Alexander Dietzius.
I Out of print. Annu. I volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.


No.


Price










MATERIALS-Continued

No. Title Price

1 22 Fabrics for Aeronautic Construction. By Sub-
committee on Standardization and Investi-
gation of Materials. (Third Annual, 1917)---------
Part 1. Cotton Airplane Fabrics.
Part 2. Balloon Fabrics.
333 Self-Luminous Materials. By N. E. Dorsey.
(Fourth Annual, 1918)--------------------------
1 34 Aluminum and Its Light Alloys. By Paul D.
Merica. (Fourth Annual, 1918)------------------
1 36 The Structure of Airplane Fabrics. By E.
Dean Walen. (Fourth Annual, 1918)-------------
3 37 Fabric Fastenings. By E. Dean Walen and R.
T. Fisher. (Fourth Annual, 1918)--------------
1 38 Airplane Dopes and Doping. By W. H. Sminith.
(Fourth Annual, 1918)-------------------------
39 The Testing of Balloon Fabrics. By Junius
David Edwards and Irwin L. Moore.
(Fourth Annual, 1918)--------------------- $0.05
Part 1. Characteristic Exposure Tests of
Balloon Fabrics.
Part 2. Use of Ultra-Violet Light for Test-
ing Balloon Fabrics.
65 The Kiln Drying of Woods for Airplanes. By
Harry D. Tiemrnan. (Fifth Annual, 1919) ----
3 66 Glues Used in Airplane Parts. By S. W. Allen
and T. R. Truax. (Fifth Annual, 1919)
3 67 Supplies and Production of Aircraft Woods.
By W. N. Sparhawk. (Fifth Annual, 1919)--------
68 The Effect of Kiln Drying on the Strength of
Airplane Woods. By T. R. C. Wilson. (Fifth
Annual, 1919)------------------------- --. 15
84 Data on the Design of Plywood for Aircraft.
By Armin Elmendorf. (Sixth Annual, 1920) -------
85 Moisture Resistant Finishes for Airplane Woods.
By M. E. Dunlap. (Sixth Annual, 1920)----------
248 The Corrosion of Magnesium and of the Mag-
nesium Aluminum Alloys Containing Manga-
nese. ByJ.A.Boyer. (Twelfth Annual,1926). .20
1 Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.








42


MATERIALS-Continued

No. Title Price

354 Aircraft Woods: Their Properties, Selection,
and Characteristics. By L. J. Markwardt.
(Sixteenth Annual, 1930)------------------- $0.20
490 The Weathering of Aluminum Alloy Sheet Ma-
terials Used in Aircraft. By Willard Mutch-
ler. (Twentieth Annual, 1934)-------------- .15

METEOROLOGY

1 4 Preliminary Report on the Problem of the At-
mosphere in Relation to Aeronautics. By
SCharles F. Marvin. (First Annual, 1915) -------
13 Meteorology and Aeronautics. By Win. R.
Blair. (Third Annual, 1917)--------------- $0. 10
Part 1. Physical Properties and Dynamics
of the Atmosphere.
Part 2. Topographic and Climatic Factors
in Relation to Aeronautics.
Part 3. Current Meteorology and Its Use.
:; 147 Standard Atmosphere. By Willis Ray Gregg.
(Eighth Annual, 1922)--------------------------
1 216 The Reduction of Airplane Flight-Test Data to
Standard Atmosphere Conditions. By Wal-
ter S. Diehl and E. P. Lesley. (Eleventh An-
nual, 1925)-----------------------------------
218 Standard Atmosphere-Tables and Data. By
Walter S. Diehl. (Eleventh Annual, 1925)--- 10
245 Meteorological Conditions along Airways. By
W. R. Gregg. (Twelfth Annual, 1926)------- 10
S246 Tables for Calibrating Altimeters and Com-
puting Altitudes Based on the Standard At-
mosphere. By W. G. Brombaclier. (Twelfth
Annual, 1926)---------------------------------
376 Some Approximate Equations for the Standard
Atmosphere. By Walter S. Diehl. (Seven-
teenth Annual, 1931)---------------------- 15
538 Altitude-Pressure Tables Based on the United
States Standard Atmosphere. By W. G.
Brombacher. (Twenty-First Annual, 1935)- .05
I Out of print. Annual volume available for referemne or loan in the Office of
Aeronautical Intelligence, National Advi-ory Committee for Aeronautics, and in
the libraries ol large cities.
A Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Inlelligenre, National Advisory Committee for Aeronautics.








43

MISCELLANEOUS

No. Title Price

308 Aircraft Accidents-Methods of Analysis. By
the Special Committee on the Nomenclature,
Subdivision, and Classification of Aircraft
Accidents, N. A. C. A. (Fourteenth Annual,
1928)----------------------------------- $0. 10
357 Aircraft Accidents-Method of Analysis. By
the Committee on Aircraft Accidents. (Six-
teenth Annual, 1930)---------------------- 10

NOMENCLATURE

1 9 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Sec-
ond Annual, 1916)------------------------------
1 15 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Third
Annual, 1917)---------------------------------
2 25 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Fourth
SAnnual, 1918)-----------------------------.----
8 91 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Sixth
Annual, 1920)----------------------------------
2157 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Eighth
Annual, 1922)---__- --------
3240 Nomenclature for Aeronautics. By Nation-
al Advisory Committee for Aeronautics.
(Twelfth Annual, 1926)--------------------------
474 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Nine-
teenth Annual, 1933)---------------------- $0. 10
NOTE-Reports 9, 15, 25, 91, 157, and 240
are obsolete.

I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.
27903-36- 4










PARACHUTES

No. Title Price

80 Stability of the Parachute and Helicopter. By
H. Bateman. (Fifth Annual, 1919)------------- ,

PROPELLERS

3 14 Experimental Research on Air Propellers. By
Win. F. Durand. (Third Annual, 1917)-----------
Part 1. The Aerodynamic Laboratory at
Leland Stanford Junior University and
the Equipment Installed with Special
Reference to Tests on Air Propellers.
Part 2. Tests on 48 Model Forms of Air
Propellers, with Analysis and Discussion
of Results and Presentation of the Same
in Graphic Form.
Part 3. A Brief Discussion of the Law of
Similitude as Affecting the Relation Be-
tween the Results Derived from Model
Forms and Those to be Anticipated from
Full-sized Forms.
119 Periodic Stresses in Gyroscopic Bodies-with I
Applications to Air Screws. By A. F. Zahm.
(Third Annual, 1917)------------------------
Part 1. The Gyroscopic Particle.
Part 2. The Gyroscopic Three-Dimensional
Body.
3 29 The General Theory of Blade Screws. By
George de Bothezat. (Fourth Annual, 1918)-------- I
30 Experimental Research on Air Propellers-III.
By Win. F. Durand and E. P. Lesley. (Fourth
Annual, 1918)------------------------------
64 Experimental Research on Air Propellers-III.
By Win. F. Durand and E. P. Lesley. (Fifth
Annual, 1919)------------------------- $0.10
71 Slip-Stream Corrections in Performance Com-
putation. By Edward P. Warner. (Fifth
Annual, 1919)..--.-------------------- .05
I out of print. Annual volume available for reference or loan In the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries nf large cities.
A Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










PROPELLERS-Continued


No. Title Price

3 109 Experimental Research on Air Propellers-IV.
By Wm. F. Durand and E. P. Lesley. (Sixth
Annual, 1920)--------------------------- ----
113 Tests on Air Propellers in Yaw. By Wm. F.
Durand and E. P. Lesley. (Seventh Annual,
1921)------------------------------------ $0. 10
141 Experimental Research on Air Propellers-V.
By Wm. F. Durand and E. P. Lesley. (Eighth i
Annual, 1922) ----------------------------- 15
3 168 The General Efficiency Curve for Air Propellers.
By Walter S. Diehl. (Ninth Annual, 1923)-- --......--.
3 175 Analysis of W. F. Durand's and E. P. Lesley's
Propeller Tests. By Max M. Munk. (Ninth
Annual, 1923) --------------------------- ------
S'177 The Effect of Slip-Stream Obstructions on Air
Propellers. By E. P. Lesley and B. M.
Woods. (Ninth Annual, 1923)-------------------
3 178 Relative Efficiency of Direct and Geared Drive
Propellers. By Walter S. Diehl. (Ninth An-
nual, 1923)-------------------------------------
3 183 The Analysis of Free-Flight Propeller Tests and
Its Application to Design. By Max M.
Munk. (Ninth Annual, 1923)--------------------
3186 Application of Propeller-Test Data to Design
and Performance Calculations. By Walter
S. Diehl. (Tenth Annual, 1924)--------_
3196 Comparison of Model Propeller Tests with the
Airfoil Theory. By W. F. Durand and E. P.
Lesley. (Tenth Annual, 1924)-----------------
220 Comparison of Tests on Airplane Propeller in
Flight with Wind-Tunnel Model Tests on Sinmi-
lar Forms. Bv W. F. Durand and E. P. Les-
ley. (Eleventh Annual, 1925)-------------- 15
'235 Interaction between Air Propellers and Airplane
Structures. By WV. F. Durand. (Twelfth An-
nual, 1926)-------------------------------------
237 Tests on Thirteen Navy Type Model Propellers.
By W. F. Durand. (Twelfth Annual, 1926)-- .10
259 Characteristics of Propeller Sections Tested in
the Variable Density Wind Tunnel. By East-
man N. Jacobs. (Thirteenth Annual, 1927)__ 10
Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.








46

PROPELLERS-Continued

No. Title Price

292 Characteristics of Five Propellers in Flight.
By J. W. Crowley, jr., and R. E. Mixson.
(Fourteenth Annual, 1928) ---------------- $0. 15
301 Full Scale Tests of Wood Propellers on a VE-7
Airplane in the Propeller Research Tunnel.
By Fred E. Weick. (Fourteenth Annual,
1928)------------------------------------ .15
302 Full Scale Tests on a Thin Metal Propeller at
Various Tip Speeds. By Fred E. Weick.
(Fourteenth Annual, 1928)----------------- 10
306 Full Scale Wind Tunnel Tests of a Series of
Metal Propellers on a VE-7 Airplane. By
Fred E. Weick. (Fourteenth Annual, 1928)-- 10
326 Tests of Five Metal Model Propellers with Va-
rious Pitch Distributions in a Free Wind
Stream and in Combination with a Model
VE-7 Fuselage. By E. P. Lesley and Elliott
G. Reid. (Fifteenth Annual, 1929)---------- 15
338 The Effect of Reduction Gearing on Propeller-
Body Interference as Shown by Full Scale
Wind Tunnel Tests. By Fred E. Weick.
(Sixteenth Annual, 1930)------------------ 15
339 Full Scale Wind Tunnel Tests with a Series of
Propellers of Different Diameters on a Single
Fuselage. By Fred E. Weick. (Sixteenth
Annual, 1930) ---------------------------- 15
340 Full Scale Wind Tunnel Tests on Several Metal
Propellers having Different Blade Forms.
By Fred E. Weick. (Sixteenth Annual, 1930)-. 10
350 Working Charts for the Selection of Aluminum
Alloy Propellers of a Standard Form to
Operate with Various Aircraft Engines and
Bodies. By Fred E. Weick. (Sixteenth
Annual, 1930).---------------------- 10
351 Full-Scale Wind Tunnel Tests of a Propeller
with the Diameter Changed by Cutting Off
the Blade Tips. Bv Donald H. Wood. (Six-
teenth Annual, 1930) -..-.-.-..-------- 15
375 Tests of Metal Propeller at High Tip Speeds.
By Donald II. Wood. (Seventeenth Annual,
1931)---------------------------------- .10










PROPELLERS-Continued

No. Title Price

378 A Comparison of Propellers having R. A. F.-6
and Clark Y Airfoil Sections. By Hugh
B. Freeman. (Seventeenth Annual, 1931)--- $0. 10
389 The Effect of Small Angles of Yaw and Pitch
on the Characteristics of Airplane Propellers.
By Hugh B. Freeman. (Seventeenth Annual,
1 1931)------------------------------------ .10
415 Tests of Nacelle-Propeller Combinations in
Various Positions with Reference to Wings.
Part I. Thick Wing-N. A. C. A. Cowled
Nacelle-Tractor Propeller. By Donald H.
Wood. (Eighteenth Annual, 1932)---------- 10
421 Measurement of the Differential and Total
Thrust and Torque of Six Full-Scale Adjust-
able-Pitch Propellers. By George W. Stickle.
(Eighteenth Annual, 1932). ---------------- 10
436 Tests of Nacelle-Propeller Combinations in
Various Positions with Reference to Wings.
Part II-Thick Wing-Various Radial-Engine
Cowlings-Tractor Propeller. By Donald H.
Wood. (Eighteenth Annual, 1932) ---------- 10
447 Static Thrust of Airplane Propellers. By
Walter S. Diehl. (Nineteenth Annual, 1933)._ 10
462 Tests of Nacelle-Propeller Combinations in
Various Positions with Reference to Wings.
Part III-Clark Y Wing-Various Radial-
Engine Cowlings-Tractor Propeller. By
Donald H. Wood. (Nineteenth Annual,
1933)------------------------------------ .10
464 Negative Thrust and Torque Characteristics of
an Adjustable-Pitch Metal Propeller. By
Edwin P. Hartman. (Nineteenth Annual,
1933) ------------------------------------ .05
481 Working Charts for the Determination of Pro-
peller Thrust at Various Air Speeds. Bvy
Edwin P. Hartman (Twentieth Annual, 1934) 10










ROTOR PLANES

No. Title Price

434 Lift and Drag Characteristics and Gliding Per-
formance of an Autogiro as Determined in
Flight. By John B. Wheatley. (Eighteenth
Annual, 1932) --------------------------$0. 05
475 Wing Pressure Distribution and Rotor-Blade
Motion of an Autogiro as Determined in
Flight. By John B. Wheatley. (Twentieth
Annual, 1934) ----------------------------.05
487 An Aerodynamic Analysis of the Autogiro Rotor
with a Comparison Between Calculated and
Experimental Results. By John B. Wheatley.
(Twentieth Annual, 1934) -------------------.05
515 Full-Scale Wind-Tunnel Tests of a PCA-2 Auto-
giro Rotor. By John B. Wheatley and Manley
J. Hood. (Twenty-First Annual, 1935) -------.05
523 The Influence of Wing Setting on the Wing Load
and Rotor Speed of a PCA-2 Autogiro as
Determined in Flight. By John B. Wheatley.
(Tweiity-First Annual, 1935) -----------------.05
536 Wind-Tunnel Tests of a 10-Foot-Diameter Gyro-
plane Rotor. By John B. Wheatley and Carl-
ton Bioletti. (Twenty-First Annual, 1935) 05

SEAPLANES

3209 Characteristics of a Single-Float Seaplane during
Take-off. By J. W. Crowley, jr., and K. M.
Ronan. (Tenth Annual, 1924)
3226 Characteristics of a Boat-Type Seaplane during
Take-Off. By J. W. Crowley, jr., and K. M.
Ronan. (Eleventh Annual, 1925)
242 Characteristics of a Twin-Float Seaplane during
Take-Off. By John W. Crowley, jr., and K.
N1. Ronan. (Twelfth Annual, 1926) ---------$0. 10
290 Water Pressure Distribution on a Seaplane
Float. By F. L. Thompson. (Fourteenth
Annual, 1928) ---------------------------- 10
328 Water Pressure Distribution on a Twin-Float
Seaplane. By F. L. Thompson. (Fifteenth
Annual, 1929)-. 10
A Out of print. Available as a separate report for reference or loan In the Office
of Aeronautical Intelligence, National Ad% isory Committee for Aeronautics.










SEA PLANES-Continued

No. Title Price

346 Water Pressure Distribution on a Flying Boat
Hull. By F. L. Thompson. (Sixteenth
Annual, 1930)---------------------------- $0. 10
453 The Estimation of Maximum Load Capacity of
Seaplanes and Flying Boats. By Walter S.
Diehl. (Nineteenth Annual, 1933)---------- .05

STABILITY AND CONTROL

'1 Report on Behavior of Airplanes in Gusts.
(First Annual, 1915)-----------------------------
Part 1. Experimental Analysis of Inherent
Longitudinal Stability for a Typical Bi-
plane. By J. C. Hunsaker.
Part 2. Theory of an Airplane Encounter-
ing Gusts. By E. B. Wilson.
1 17 An Investigation of the Elements which Con-
tribute to Statical and Dynamical Stability,
and of the Effects of Variation in those Ele-
ments. By Alexander Klemin, Edward P.
Warner, and George M. Denkinger. (Third
Annual, 1917)------------------------------
1 21 Theory of an Airplane Encountering Gusts-II.
By E. B. Wilson. (Third Annual, 1917)-----------
3 26 The Variation of Yawing Moment Due to Roll-
ing. By E. B. Wilson. (Fourth Annual,
1918)------------------------------------------
3 27 Theory of an Airplane Encountering Gusts-III.
By E. B. Wilson. (Fourth Annual, 1918)----------
a 95 Diagrams of Airplane Stability. By H. Bate-
men. (Sixth Annual, 1920)---------------------
1 96 Statical Longitudinal Stability of Airplanes.
By Edward P. Warner. (Sixth Annual, 1920) ------
3112 Control in Circling Flight. By F. H. Norton
and E. T. Allen. (Seventh Annual, 1921)_------
'120 1 Practical Stability and Controllability of Air-
planes. By F. H. Norton. (Seventh Annual,
1921)----------------------------------
'Out of print. Annual volume available for reference or ioan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
S Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics.










STABILITY AND CONTROL-Continued


No.


Title


Price


3153 Controllability and Maneuverability of Air-
planes. By F. H. Norton and W. G. Brown.
(Eighth Annual, 1922)-----------------------
' 172 Dynamic Stability as Affected by the Longi-
tudinal Moment of Inertia. By Edwin B.
Wilson. (Ninth Annual, 1923)-----------------
3 293 Two Practical Methods for the Calculation of
the Horizontal Tail Area Necessary for a
Statically Stable Airplane. By Walter S.
Diehl. (Fourteenth Annual, 1928)- -------
298 Effect of Variation of Chord and Span of Aile-
rons on Rolling and Yawing Moments in
Level Flight. By R. H. Heald and D. L.
Strother. (Fourteenth Annual, 1928)------- $0. 10
343 Effect of Variation of Chord and Span of Aile-
rons on Rolling and Yawing Moments at
Several Angles of Pitch. By R. H. Heald,
D. H. Strother, and B. H. Monish. (Sixteenth
Annual, 1930)------------------------ 15
379 Rolling Moments due to Rolling and Yaw for
Four Wing Models in Rotation. By Mont-
gomery Knight and Carl J. Wenzinger.
(Seventeenth Annual, 1931)--------------- 15
386 Maneuverability Investigation of an F6C-4
Fighter Airplane. By C. H. Dearborn and H.
W. Kirschbaum. (Seventeenth Annual, 1931)_ .20
393 Span-Load Distribution as a Factor in Stability
in Roll. By Montgomery Knight and Richard
W. Noyes. (Seventeenth Annual, 1931)---- 10
442 A Comparison between the Theoretical and
iMeasured Longitudinal Stability Charac-
teristics of an Airplane. By Hartley A.
Soil6 aind John B. W heatlev. (Nineteenth
Annual, 1933) ---------------------------- 05
457 Maneuverability Investigation of an "03U-1"
Observattion Airplane. By F. L. Thompson
and H. W. Kirschbaum. (Nineteenth An-
Snual. 1933---------.--------------------- .05
467 The Experimental Determination of the Mo-
mIents of Inertia of Airplanes. By Hartley
A. Soul6 and Marvel P. Miller. (Nineteenth
Annual, 1933)------.--.-------------------. 05
1 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, Nationul Advisory Committee for Aeronautics.










STABILITY AND CONTROL- Continued

No. Title Price

484 A Flight Investigation of the Effect of Mass
Distribution and Control Setting on the Spin-
ning of the XN2Y-1 Airplane. By N. F.
Scudder. (Twentieth Annual, 1934) -----$0. 05
521 An Analysis of Longitudinal Stability in Power-
Off Flight with Charts for Use in Design.
By Charles H. Zimmerman. (Twenty-First
Annual, 1935) ---------------------------- 10
548 Effect of Tip Shape and Dihedral on Lateral-
Stability Characteristics. By Joseph A.
Shortal. (Twenty-Second Annual, 1936)-----: .00
i

STRENGTH OF CONSTRUCTION

1 3 Report on the Investigations of Aviation Wires
and Cables, Their Fastenings and Terminal
Connections. By John A. Roebling's Sons
Co. (First Annual, 1915)-----------------------
3 35 The Strength of One-Piece, Solid, Built-Up, and
Laminated Wood Airplane Wing Beams.
By John H. Nelson. (Fourth Annual, 1918) ------
3 76 Analysis of Fuselage Stresses. By Edward P.
Warner and Roy G. Miller. (Fifth Annual,
1919)----------------------------------------
3 82 Airplane Stress Analysis. By A. F. Zahm.
(Fifth Annual, 1919)---------------------------
3 92 Analysis of Wing Truss Stresses. By Edward '
P. Warner and Roy G. Miller. (Sixth Annual,
1920)-----------------------------------------
3104 Torsion of Wing Trusses at Diving Speeds.
By Roy G. Miller. (Sixth Annual, 1920)----------
137 Point Drag and Total Drag of Navy Struts
No. 1 Modified. By A. F. Zahm, R. H.
SSmith, and G. C. Hill. (Eighth Annual, 1922)_ $0. 05
3 140 Lift and Drag Effects on Wing Tip-Rake. By
A. F. Zahm, R. M. Bear, and G. C. Hill.
(Eighth Annual, 1922)--------------------------
I Out of print Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
I Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










STRENGTH OF CONSTRUCTION-Continued

No. Title Price

3143 Analysis of Stresses in German Airplanes. By
Wilhelm Hoff. (Eighth Annual, 1922)
3 145 Internal Stresses in Laminated Construction
By A. L. Heim, A. C. Knauss, and Louis.
SSeutter. (Eighth Annual, 1922)-------------.----.
3161 The Distribution of Lift over Wing Tips and
Ailerons. By David L. Bacon. (Ninth
Annual, 1923)---------------------------------
2180 The Influence of the Form of a Wooden Beam
on Its Stiffness and Strength-I: Deflection
of Beams with Special Reference to Shear
Deformations. Bv J. A. Newlin and G. W.
Trayer. (Ninth Annual, 1923)-------------------
8181 The Influence of the Form of a Wooden Beam
on Its Stiffness and Strength-II: Form
Factors of Beams Subjected to Transverse
Loading Only. By J. A. Newlin and G. W.
Trayer. (Ninth Annual, 1923)-------------------
:I$S The Influence of the Form of a Wooden Beam
on Its Stiffness and Strength-III: Stresses
in Wood Members Subjected to Combined
Column and Beam Action. By J. A. Newlin
and G. W. Trayer. (Tenth Annual, 1924)---------
214 Wing Spar Stress Charts and Wing Truss
Proportions. By Edward P. Warner. (Elev-
enth Annual, 1925)---------------------- $0. 10
251 Approximations for Column Effect in Airplane
Wing Spars. By Edward P. Warner and
Mac Short. (Twelfth Annual, 1926)-------- 10
329 The Torsional Strength of Wings. By C. P.
Burgess. (Fifteenth Annual, 1929)---------- 10
334 The Torsion of Members Having Sections
Common in Aircraft Construction. By
George W. Trayer and I1. W. March. (Fif-
teenth Annual, 1929)---------------------- .25
344 The Design of Plywood Webs for Airplane Wing
Beams. By George W. Trayer. (Sixteenth
Annual, 1930)---------------------------- 10
345 The Design of Airplane Wing Ribs. By J. A.
Newlin and George W. Trayer. (Sixteenth
Annual, 1930)--.------------------------ 25
Out of print. Available as a separate report for reference or loan In the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










STRENGTH OF CONSTRUCTION-Continued

No. Title Price

347 A Method of Calculating the Ultimate Strength
of Continuous Beams. By J. A. Newlin and
Geo. W. Trayer. (Sixteenth Annual, 1930)-- $0. 10
348 Strength of Welded Joints in Tubular Members
for Aircraft. By H. L. Whittemore and
W. C. Brueggeman. (Sixteenth Annual, 1930). .30
356 Strength of Rectangular Flat Plates under Edge
Compression. By Louis Schuman and Goldie
Back. (Sixteenth Annual, 1930)------------- 15
382 The Elastic Instability of Members having
Sections Common in Aircraft Construction.
By George W. Traver and H. W. March.
(Seventeenth Annual, 1931)---------------- .25
473 Strength Tests of Thin-Walled Duralumin
Cylinders in Compression. By Eugene E.
Lundquist. (Nineteenth Annual, 1933)_ 10
479 Stability of Thin-Walled Tubes under Torsion.
ByL.:H.Donnell. (Twentieth Annual, 1934)_ .10
491 Vibration Response of Airplane Structures. By
T. Theodorsen and A. G. Gellalles. (Twenti-
eth Annual, 1934)------------------------- 10
508 Analysis of 2-Spar Cantilever Wings with Special
Reference to Torsion and Load Transference.
By Paul Kuhn. (Twenty-First Annual, 1935)_ .10
509 General Equations for the Stress Analysis of
Rings. By Eugene E. Lundquist and Walter
F. Burke. (Twenty-First Annual, 1935) ----- 05

WIND TUNNELS AND LABORATORIES

3 44 The Altitude Laboratory for the Testing of I
Aircraft Engines. By H. C. Dickinson and
H. G. Boutell. (Fourth Annual, 1918)------------
72 Wind-tunnel Balances. By Edward P. Warner
and F. H. Norton. (Fifth Annual, 1919)_....._ $0. 10
8 73 The Design of Wind Tunnels and Wind-tunnel
Propellers. By Edward P. Warner and F.
H. Norton. (Fifth Annual, 1919)----------- ------
'Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










WIND TUNNELS AND LABORATORIES-Continued

No. Title Price

3 74 Construction of Models for Tests in Wind Tun-
nels. By F. H. Norton. (Fifth Annual,
1919)--------------------------------------
3 98 1 Design of Wind Tunnels and Wind-Tunnel
Propellers-IL. By F. H. Norton and Ed-
Sward P. Warner. (Sixth Annual, 1920)-----------
3 146 The Six-Component Wind Balance. By A. F.
I Zahm. (Eighth Annual, 1922)------------------
195 Standardization Tests of N. A. C. A. No. 1
Wind Tunnel. By Elliott G. Reid. (Tenth
SAnnual, 1924)---------------------------- $0. 10
227 The Variable-Density Wind Tunnel of the
National Advisory Committee for Aeronau-
tics. By Max M. Munk and Elton W. Miller.
(Eleventh Annual, 1925)------------------- .10
3231 Investigation of Turbulence in Wind Tunnels by
a Study of the Flow About Cylinders. By
H. L. Dryden and R. H. Heald. (Eleventh
Annual, 1925)---------------------------------
275 The Effect of the Walls in Closed Type Wind
Tunnels. By George J. Higgins. (Thirteenth
Annual, 1927)-------------- ------------- 10
300 The Twenty-Foot Propeller Research Tunnel of
the National Advisory Committee for Aero-
nautics. By Fred E. Weick and Donald H.
Wood. (Fourteenth Annual, 1928)--------- .10
322 Investigation of Air Flow in Open Throat Wind
Tunnels. By Eastman N. Jacobs. (Fifteenth
Annual, 1929)----------------------------- 10
342 Effect of Turbulence in Wind Tunnel Measure-
ments. By H. L. Dryden and A. M. Kuethe.
(Sixteenth Annual, 1930) ------------------ 10
387 The Vertical Wind Tunnel of the National
Advisory Comzmittee for Aeronautics. By
Carl J. WVenzinger and Thomas A. Harris.
(Seventeenth Annual, 1931).--------------- 10
392 Reduction of Turbulence in Wind Tunnels.
Byv Hugh L. Dryden. (Seventeenth Annual,
1931)--------- ------------------- 10
I Out of print. Available as a separate report for reference or loan in the Office
.f Aeronautical Intelligence, National Advisory Committee for Aeronautics.






D5

WIND TUNNELS AND LABORATORIES-Continued

No. Title Price

410 The Theory of Wind-Tunnel Wall Interference.
Theodore Theodorsen. (Eighteenth Annual,
t932)----------------------------------- $0. 10
412 The 7- by 10-Foot Wind Tunnel of the National
Advisory Committee for Aeronautics. By
I Thomas A. Harris. (Eighteenth Annual, 1932). .10
416 The N. A. C. A. Variable-Density Wind Tunnel.
Bv Eastman N. Jacobs and Ira H. Abbott.
(Eighteenth Annual, 1932)------------------- .05
459 The N. A. C. A. Full-Scale Wind Tunnel. By
Smith J. De France. (Nineteenth Annual,
1933)------------------------------------ .05
461 Interference on an Airfoil of Finite Span in an
Open Rectangular Wind Tunnel. By Theo-
doreTheodorsen. (Nineteenth Annual, 1933)__ .05
463 The N. A. C. A. High-Speed Wind Tunnel and
Tests of Six Propeller Sections. By John
Stack. (Nineteenth Annual, 1933)_- .------- .10
470 The N. A. C. A. Tank-A High-Speed Towing
Basin for Testing Models of Seaplane Floats.
Bv Starr Truscott. (Nineteenth Annual,
1933-------------------- ----------------- .10
478 Experimental Verification of the Theory of
Wind-Tunnel Interference. By Theodore
Theodorsen and Abe Silverstein. (Twentieth
Annual, 1934)----------------------------- .10
524 A Turbulence Indicator Utilizing the Diffusion
of Heat. By G. B. Schubauer. (Twenty-
First Annual, 1935)----------------------- .05
547 Wind-Tunnel Interference with Particular Refer-
ence to Off-Center Positions of the Wing and
to the Downwash at the Tail. By Abe Silver-
stein and James A. White. (Twenty-Second
Annual, 1936)-------------------.--------
















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